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SDI Ground Vehicles Catalog [DO NOT POST]

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SDI Ground Vehicles Catalog [DO NOT POST]

Postby The Technocratic Syndicalists » Sat Apr 23, 2016 10:40 pm

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PzKpfw 151 Tiger

General Characteristics:
  • Type: Main battle tank
  • Weight: 72.5 t
  • Length (hull): 7.9 m
  • Length (gun forward): 12.4 m
  • Width: 3.8 m
  • Height (turret roof): 2.6 m
  • Crew: 3 (driver, gunner, commander)

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,300 l
  • Operational range: 550 km

Armament:
  • 1x 15 cm L/60 smoothbore gun, 39 rounds
  • 2x 8 mm MG-45E machine guns, 5,850 rounds

Maneuverability:
  • Power/weight Ratio: 33.5 PS/t (24.6 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.90 kg/cm2
  • Gradient: 70%
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
The Panzerkampfwagen 151 (PzKpfw 151) Tiger is an advanced main battle tank (MBT) designed by SDI Vehicle Systems.


Armament:
Main gun: The main armament of the Tiger is a 15 cm SDI smoothbore gun with a barrel length of 60 calibers which is designed to fire SDI's family of 15 cm high-pressure smoothbore ammunition.The gun is mounted in the vehicle's stabilized turret and is capable of traversing a full 360° at 40°/s and elevating from -10° to +15° at 40°/s using an electric turret drive with < 0.3 mrad pointing accuracy. The 15 cm L/60 gun includes a hydraulic recoil system with approximately 500 mm of travel along with a slotted multi-baffle muzzle brake to absorb the recoil force of the weapon. The gun uses a vertically opening multi-lug breech design designed to reduce the stress concentrations between the breech and breech-block during firing. The nickel-chromium-molybdenum alloy steel lugs on either side of the breech mechanism are subject to both shot peening and mechanical overload to further induce favorable residual stresses into the lugs, maximizing the the number of firing cycles the breech mechanism can endure before needing replacement. To reduce barrel weight the 15 cm L/60 gun features a composite construction consisting of an autrofrettaged double vacuum remelted ultra-high strength steel (UHSS) tube with a metal-matrix (MMC) composite overlap made from silicon carbide fibers transversely wound into a 6061 aluminum alloy matrix. High temperature wear and corrosion protection for the gun tube assembly is via twin refractory tantalum liners along the inside of the barrel applied using a sputtering process. Barrel weight of the cannon is approximately 1,600 kilograms and the complete weight of the barrel with the breech and gun mount assembly is approximately 4,300 kilograms. A full-length composite thermal sleeve constructed from E-glass filaments transversely wound into a low thermally conductive epoxy matrix is attached via a pivoting collar to the bore evacuator, the thermal sleeve serving to minimize barrel distortion due to uneven heating of the barrel surface and to minimize the thermal signature of the barrel assembly. Accuracy degradation due to terrain-induced vibrations on the gun are minimized using a dynamically tuned shroud (DTS), a spring loaded collar with an energy absorbing rubber liner attached to the front of the thermal sleeve which acts as a tuned mass absorber. The absorber is dynamically tuned using a set of preloaded leaf springs which can be adjusted to vary the stiffness of the absorber. This system allows the gun to be isolated from external vibrations and also reduces the load transmitted from the gun barrel to the projectile during launch, significantly improving weapon accuracy. The gun is also fitted with a dynamic muzzle reference system (MRS) comprising a reflector mounted on the muzzle and a laser transmitter mounted on the rotor assembly which automatically measures the angular deflection of the barrel in both azimuth and elevation in real time while the tank is both stationary and moving. The DMRS is connected to the firing circuit of the gun and when the gunner depresses the trigger will automatically fire the gun only when the barrel is near straight, maximizing accuracy.

Autoloader: The tank's cannon is fed from a bustle-mounted robotic autoloader system (RALs) which contains 17 ready rounds in the rear of the turret. The RALS system comprises a a double-row, closed-loop chain of 17 telescoping cells each containing a single 15 cm round. When an ammunition type is selected by the gunner the chain drive moves the telescoping cell with the cartridge into the loading port where the loading door in-line with the breech of the gun is opened. An electric rammer then grips the rim of the round and then pushes the round through the telescoping cell into the gun breech, the rammer and telescoping cell then retracting back into the bustle and the loading door closed. With the process reversed rounds can be extracted from the breach and put back in the autoloader by the system. Twin titanium blowout panels are fitted to the top of the RALs system to protect the crew in the event of of an ammunition explosion. Reloading of the RALS system can be done manually using a reloading port at the rear of the vehicle. 22 rounds of 15 cm two-piece ammunition are stored separately in the hull in twin 17 cell, double-row closed-loop chain (like those in the turret bustle) magazine units stacked on top of each other which are located in between aft end of the turret ring and the transversely mounted powerpack. Each cell in the hull magazine contains either a forward projectile section or two aft propellant charges, allowing up to 22 complete rounds to stored separately in the hull magazine. A robotic transfer mechanism is used to shift ammunition from the lower hull autoloader magazine to the upper hull magazine and from the hull magazine into the turret bustle autoloader. Reloading the turret magazine from the bustle takes approximately two minutes and requires the vehicle to be stationary with the turret locked facing forward. Replenishment of the hull magazines is via a port located on the left rear of the turret which transfers rounds directly into the turret bustle autoloader cells and then into the twin hull magazines using the robotic transfer arm.

Smoke-grenade launchers: The vehicle is equipped with a total 32 smoke grenade launchers grouped into four groups of four on each turret face turret covering the front two 90° sectors. The smoke launchers fire 76 mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual (0.4 to 0.7 µm) and infrared (0.7 to 14 µm) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. Each smoke grenade weighs 1.2 kg including 800 grams of red phosphorous fill and is launched to a range of 40-45 meters where the grenade bursts and produces a smokescreen approximately 12 meters long and 6 meters high for a duration of 20-30 seconds. The launchers can also fire fragmentation grenades containing an explosive charge and 750 grams of steel balls which are designed to burst at a height of 5-6 meters above the ground. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each frontal 90° sector.

Secondary armament: Two belt-fed 8mm MG 45E machine guns are fitted as standard to the tank. A coaxial MG-45E machine gun is mounted on the left side of the main gun and another MG 45E machine gun is mounted mounted to a remote weapon station attached to commander's sight on top of the turret. 5,850 rounds of 8x57mm ammunition and carried inside the vehicle for both weapons.


Protection:
Armor Protection:The Tiger employs a heavy-metal composite armor system designed to provide protection against kinetic energy (KE) threats in the form of long-rod penetrators fired by high-pressure tank cannons and chemical energy (CE) threats including large-caliber shaped charge munitions. The composite armor covers the front and sides of the turret and the front and the sides of the hull with the remainder of the vehicle protected only by conventional steel armor. The line-of-sight thickness of the armor of the vehicle measures 1,300 mm across the glacis and turret front and 700 mm across the frontal turret sides. The armor is designed to provide frontal /- 30° protection against large caliber tank gun fired APFSDS rounds (800-1000 mm RHA penetration) and large caliber anti-tank guided missiles (~170 mm diameter SC with 1500-1600 mm RHA penetration) and 360° protection against 15mm AP ammunition and handheld anti-tank weapons (110 mm diameter SC). Approximate average RHA equivalent protection for the glacis and turret armor across the frontal 60 degree arc is 1,000-1,200 mm RHA against kinetic-energy munitions and 1,800-2,200 mm versus chemical-energy munitions. The armor in the glacis is structurally integrated into the hull and side skirts of the vehicle while the turret composite armor is contained in a series of armor modules which bolt onto the front and sides of the turret. The armor modules are designed to be replaced in field when damaged and can additionally be opened up and specific armor components inside the modules repaired or replaced in the field. In the addition to the composite armor the inside of the hull and the turret of the vehicle are fitted with spall panels to minimize the post-armor effects of rounds which penetrate into the vehicle. The spall panels are also loaded with 5% by weight boron to provide protection against fast neutron, thermal neutron, primary gamma rays and secondary gamma rays.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment underneath the main gun.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously online begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: The Tiger is equipped with SDI Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT projectiles. The system consists of a set of pre-warner radar arrays and multiple modular countermeasure modules mounted along the turret sides and roof containing electro-optical tracking sensors and directional explosive countermeasures designed to destroy or deflect oncoming projectiles before they strike the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. Six panels are arranged around the sides of the turret with another two on the turret roof which provide combined 360 degree hemispherical coverage around the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are contained in bricks on the outside of the vehicle and employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) heavy metal tungsten alloy (HMTA) shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the turret to provide coverage over the the hull of the vehicle by steering the blast downwards or to defeat over-fly top attack projectiles by firing upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past four or so meters from the vehicle. The countermeasures bricks themselves employ a metal-free composite construction and are encased in a layer of thermoplastic armor to prevent the brick itself from generating any shrapnel and to protect the explosive charges from small arms fire and shrapnel and other hazards. The vehicle by default is fitted with eight countermeasure modules along the sides and front of the turret which provide coverage around the the hull and turret sides against direct attack or over-fly top-attack projectiles and an additional four roof-mounted countermeasure modules to intercept diving top-attack munitions.


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel

The Tiger is powered by a self contained rear drive system which includes an AMG (Arkaenisch Motorenfabrik Gesellschaft) designed HL280 diesel engine and an AMG AK 7-700 hydromechanical planetary transmission, accessory drive gearbox, auxiliary power unit (APU), self-cleaning air filter (SCAF), exhaust IR suppression system, engine and APU fuel system, and the vehicle electrical system which is separated from the fighting compartment by a fireproof bulkhead. Inlet air for the engine flows through a set of armored grills located on the left side of the vehicle's engine deck before being scrubbed by a pre-cleaner and passed through a self-cleaning air filter (SCAF) where the now cleaned air then enters the engine. The exhaust from the engine is passed through an IR suppression system and then finally vented overboard through a louvered grill mounted at the rear of the vehicle. Relatively compact and designed for reliability and ease of maintenance, the vehicle's power pack has a 5,000 hour mean time between overhaul (MTBO) and air filters designed for 100 hour continuous operation at twice zero-visibility dust concentrations, can accept virtually any grade of diesel or jet fuel, can cold start at temperatures as low as -50 degrees C, and can be removed from the vehicle in as little as 15 minutes for replacement or repair.

Engine: The AMG designed HL280 diesel engine is a multi-fuel, low-heat rejection (LHR), quad-turbo diesel engine with a maximum power output of 1,765 kilowatts (2,400 PS) at its maximum rated speed of 3,300 RPM. The HL280 engine block is a monobloc design with a 60 degree cylinder bank angle and is constructed from compacted graphite iron (CGI) and features integral charge air cooler and intake manifold housings along with machined cooling passages for the synthetic oil coolant. Both the turbocharger intercooler and aftercoolers and exhaust manifolds are constructed from high-temperature stainless steel alloy and are located on the outside of the V-block with the intake manifolds integral to the V-block itself. The HL280 features a common rail electronic controlled injection (ECI) system with one piezoelectric injector per engine cylinder. Fuel is pressurized by a high-pressure, fuel lubricated hydraulic boost pump with the fuel rail mounted on the engine serving as a high-pressure accumulator. The fuel is distributed to the individual fast-switching piezoelectric injectors integrated into each engine cylinder where fuel is then injected at 2,500 bar pressure into each engine cylinder. The cylinder heads are constructed from cast ductile iron and feature black nitride coated stainless steel inlet valves and high temperature titanium/inconel alloy exhaust valves with monolithic zirconia valve seats capable of surviving the high exhaust gas temperatures of each cylinder without needing cooling. The piston in each cylinder is two piece, articulated design with a forged maraging steel crown with tungsten-carbide piston rings screwed into an aluminum skirt assembly, the steel crown of the piston being cooled using a single piston oil supply nozzle located on the underside the crown. Both the cylinder head and piston crown feature a plasma-spray applied 2mm zirconia ceramic thermal barrier coating (TBC) which facilitates high temperature, high pressure engine operation with minimal thermal losses. The cylinders themselves are constructed from ductile cast iron with a silicon carbide (SiC) fiber reinforced 7075 aluminum alloy metal matrix composite liner with a diamond-like carbon (DLC) coating which reduces both the head temperature and the friction between the piston rings and the cylinder walls. The cylinders are cooled using synthetic oil which flows through an annular groove at the top of the cylinder in between the cylinder block and cylinder liner. The engine's crankshaft and connecting rods use an induction hardened, forged 18Ni maraging steel alloy construction with diamond-like carbon (DLC) coatings to improve abrasion and corrosion resistance. The connecting rods are a telescoping design which allows for the compression ratio of the engine to be varied from 9 up to 18, allowing for the cycle isotropic efficiency to be maximized across the engine's entire operating envelope. The intake pressure of the HL280 engine is boosted via the use of four variable-geometry sequential turbochargers. The turbine of each turbocharger is a single, stage axial design constructed from silicon nitride ceramic and features a set of axially pivoting variable-area turbine vanes which open up at low engine RPMs to reduce turbo-lag and increase engine torque and then at higher engine RPMs close down to increase engine boost pressure. The exhaust turbine of each turbocharger drives both a low pressure compressor (LPC) and high pressure compressor (HPC) on a common shaft with an air-oil intercooler placed between the low pressure and high pressure stages and an air-oil aftercooler placed after the high-pressure stage of each turbocharger. Each turbocharger additionally features set of variable inlet guide vanes (VIGVs) ahead of low and high pressure compressors which prevent surge or chocking of the flow through the compressor.

Transmission: The transmission used with the HL280 engine is the AMG AK 7-700 hydro-kinetic power shifting, reversing, and steering transmission with seven forward and three reverse gears. The transmission employs a powershift system with planetary gearing capable of shifting under full engine load, a reversing gear mechanism, and a hydrokinetic torque converter with a lock-up clutch to improve efficiency at higher speeds. Operation of the transmission is fully automatic and automatically changes gear within a range pre-selected by the driver. A digital transmission control unit (TCU) is used to control shifting in automatic mode which interfaces with the engine control unit (ECU) to control the range of the transmission. A manual override is additionally fitted which allows for range override of the transmission through a lever in the driver's compartment connected through a cable to a series of mechanical linkages attached to the shifting mechanism of the transmission. The steering drive fitted to the transmission is an infinitely variable hydrostatic/hydrodynamic superimposed differential system employing twin hydraulic drives with variable-displacement hydraulic pumps and twin hydraulic motors which are used to add or subtract power from each side of the vehicle and allow for neutral or pivot turning at infinitely variable speed. Power is transferred to each sprocket using a twin-speed planetary final drive with 10:1 and 20:1 gear ratios. Braking functions of the transmission include a combined hydrodynamic/mechanical dual circuit integrated brake system with an internal hydrodynamic brake and external oil-cooled power assisted disc brakes on either side of the transmission. Independent service and parking brakes are additionally included. A hydraulic power take-off (PTO) system fitted to the transmission output is used to power the transmission cooling fans as well the accessory drive gearbox which contains a toroidal CVT (continuously variable transmission) which provides a constant 3,000 rpm speed output independent of engine RPM which is used to drive the vehicle's NBC compressor, alternator, self-cleaning air filter (SCAF), scavenge blower, and IR exhaust suppression system.

Auxiliary Power Unit: Auxiliary power is provided via an SDI RKM700 under-armor auxiliary power unit (APU) attached to the accessory gearbox within the engine compartment. The APU system consists of the RKM700 engine along with integral starter, fuel conditioning system, and self-contained cooling system and is used to power the vehicle's alternator, air filter compressor, and self-cleaning air filter while the engine is offline. The RKM700 APU is a single-cylinder turbocharged rotary engine with a 0.7 liter displacement which can generate a maximum of 60 kilowatts (80 PS) of power at it's rated speed of 6,000 RPM. In addition to the single-stage turbocharger the RKM700 engine features an air-to-air aftercooler and a dry-sump oil lubrication system. The RKM700 APU is oil-cooled using an integral oil-air heat exchanger and cooling fan. The APU is fed from the main engine air inlet and exhausts though a grille in the upper left hull sponson.

Electrical System The vehicle's electrical system interfaces with the engine and transmission, CVT accessory drive gearbox, self-cleaning air filter (SCAF,) APU, NBC filtration system, HVAC system, fuel system, and fire suppression system. The electrical system is consists of four 170 amp-hour lithium-ion batteries, battery heater system, electrical distribution system, and a 1,000 amp, 28 kilowatt oil-cooled brushless permanent magnet alternator driven by the APU or main engine through the CVT accessory drive gearbox. The lithium-ion batteries are wired in series-parallel and provide 680 amp-hours capacity of 24 VDC output from -40 degrees to +50 degrees C ambient temperature and allow for engine cold start at -40 C without the APU after up to four hours of silent watch. The batteries are charged using the 1,000 amp oil-cooled alternator through a solid-state voltage regulator which at an alternator speed of 3,000 rpm delivers 28-30 volts of DC power at up to 150 amps to rapidly charge the batteries.

Suspension & Running Gear: the Tiger features an SDI designed semi-active in-arm hydro-pneumatic suspension system with four sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (16 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The suspension also allows the vehicle to "tilt" forwards or backwards permitting additional gun elevation and depression. The vehicle uses a decoupled running gear design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle employs double-pin, twin center guide tracks with removable rubber road-pads. Track width is 75 centimeters with a pitch of 20 centimeters with a total of 88 links per track. To reduce weight the vehicle's track links and pins employ a novel composite construction using a particle reinforced titanium metal matrix composite in place of traditional steel. The track parts are formed through powder metallurgy using titanium carbide (TiC) particles mixed into Ti-6Al-6V-2Sn (Ti-6-6-2) alloy powder, the final composite parts offering superior corrosion and wear resistance to steel parts while reducing track weight approximately 25% over an equivalent strength steel design. Each track link is fitted standard with twin detachable road pads constructed from a kevlar-natural rubber composite to reduce noise and road wear. For traversing icy ground up to 44 steel cleats can be fitted to each track, one cleat replacing the rubber pad on every fifth track link, the cleats being stored on the vehicle's glacis when not in use. The tank's sixteen road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units.


Fire Control:
Gunner's Sight: The Tiger is equipped with a two-axis stabilized gunner's thermal sight which is housed in an armored covering at the right forward edge of the turret. The main features of the sight are a third generation dual-wavelength (3-5 um and 8-12 um) thermal imager and high-resolution color CCD imager with 2-axis independently stabilized line of sight, ballistic computer, eye-safe laser rangefinder, and integrated GPS/inertial navigation system. The third generation thermal imager used with the gunner's sight is a SDI'd WBG-3G 1280 x 1024 pixel dual color (MWIR and LWIR) Mercury cadmium telluride (HgCdTe) staring focal plane array (FPA) detector. The thermal imager is cooled using a Stirling cycle linear drive cryocooler which cools the detector assembly to 77° K. The detector and crycooler system are contained in a single Standard Advanced Dewar Assembly (SADA), a closed-cycle dewar-cooler assembly containing the linear crycooler, infrared FPA, Dewar, and various control electronics and sensors. The dual-color thermal imager features a color fusion system which assigns colors to pixel values from each MWIR and LWIR band (red for LWIR, cyan for MWIR), adding color contrast to the otherwise black-and-white thermal image. The thermal sight can be toggled between 16.7° wide field of view (WFOV), 8.9° medium field of view (MFOV), 4.4° narrow field-of view (NFOV), and 2.2° ultra-narrow field of view settings. Mounted alongside the thermal imager is a 2048 x 1536 pixel visible/near IR monochrome CCD camera with selectable 16.7° wide field of view (WFOV), 8.9° medium field of view (MFOV), 4.4° narrow field-of view (NFOV), and 2.2° ultra-narrow field of view settings which provides the gunner's sight with an additional daylight channel in addition to the dual-band thermal channel. Detection, recognition, and identification ranges for the sight are around 22/12/7.5 km for the thermal channel and 24/15/9 km for the daylight channel against a 2.3 x 2.3 meter vehicle target. An image fusion function is also available combines the data from the dual-band thermal imager and the CCD camera to provide a fused image selectable on the sight control panel from 100% visible / 0% IR to 0% visible / 100% IR in infinitely variable increments. Range information for the fire-control system is provided by a 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder which provides+/- 1 meter accuracy from ranges of 50 meters up to 40 kilometers. The sight additionally contains a 1.064 um laser designator, laser illuminator and laser spot tracker. The sight's dual axis stabilized head mirror assembly provides for enhanced on-the-move (OTM) stabilization capability, ensuring the reticle of the sight stays stabilized in the center of the sight while the vehicle is on the move. Dual-axis stabilization is provided by micromachined 2-axis hemispherical Resonator Gyroscopes (HRGs) with 0.001 deg/hour drift capability integrated into the sights inertial measurement unit (IMU) system. The output from the gunner's sight is displayed in the gunner's binocular image control unit (BICU), a dual binocular display mounted in the gunner's station which generates a stabilized virtual image of the output of the sighting unit. The display from the gunner's sight is also displayed in the gunner's primary sight extension (GPSE) in the commander's station which allows the commander to see what the gunner is looking at and to potential override him or sight and fire the main gun, if necessary. A backup TZF-18 gunner's auxiliary sight is mounted coaxially with the main armament and can be used to aim and fire both the main gun and coaxial machine gun armament. The TZF-18 is a fixed 8x magnification sight with a 10 constructed from a pressurized aluminum housing and features diopter adjustment, a tritium illuminated reticle with stadiametric rangefinder, and selectable neutral-density (NS) filter for high-brightness conditions.

The gunner's sight is integrated with a GPS/INS navigation system which inputs accurate heading, attitude, velocity and position information of the vehicle into the sight's ballistic computer. The navigation system combines 3 axis fiber optic gyroscopes, 3 axis pendulous accelerometers, and digital magnetic compass with further sensor input from vehicle motion sensor (VMS) systems in the drivetrain and two lightweight DGPS antennas integrated into either side of the sight housing. Attitude information from the GPS is used to give the sight far target location (FTL) capability which combines data from the GPS/INS system and laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The ballistic computer for the gunner's sight is contained in a single line replaceable unit (LRU) and features a shock, radiation, and electro- static discharge hardened outer casing and a convection cooling system with -50 to +70° C operating capability. The ballistic computer synthesizes inputs from multiple sensors including laser rangefinder, barrel temperature sensors and dynamic muzzle reference system (MRS), crosswind sensor, RFID propellant temperature sensors, vehicle motion sensors (VMS), and inertial navigation and vehicle position sensors and takes into account the target range, vehicle cant angle, the direction of vehicle motion relative to the target, crosswind velocity and direction, and the ballistic data of the selected ammunition in order to calculate the required lead and elevation to hit the target. The firing solution is then automatically transferred to the main gun's stabilization and control system which then lays the main gun onto the line-of-sight of the gunner's sight. The gunner's sight also features an automatic target recognition (ATR) capability imaging through an SDI designed imaging sensor autoprocessor (ISA) unit built into the sight. The ISA employs parallel very high speed integrated circuit (VHSIC) processors contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the sight's dual-band FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, helicopters, and other vehicles.

Commander's Sight: External vision for the commander is provided by the commander's sight which features the same infrared imager, color CCD camera, laser range finder as the gunner's sight. The commander's sight features independent dual-axis HRG stabilization along with servomotor actuated 360° azimuth and -13°to +70 ° elevation travel. The independent commander's sight gives the vehicle "hunter-killer" capability by allowing the commander to independently search for targets and then hand them off to the gunner for engagement. Like the gunner's sight the commander's sight is contained within an armored housing which protects the assembly against shrapnel and small arms fire. The commander's sight additionally includes track-while-scan capability and an integral ballistic computer and ATR processor identical to the one in the gunner's sight which enables lead angle computation capability and far-target location ability like that of the gunner's sight. The commander's sight features both manual and automatic scan settings and a gun line of sight (GLOS) mode which slaves the main gun to the commander's sight. High Definition video output from the commander's sight is transferred into the turret via a 100 MHz bandwidth fiber-optical slip ring and displayed on the commander's integrated display (CID), a 1920 x 1080 resolution touchscreen SXGA display with 20 programmable edge keys all with variable backlight which can each be assigned to various surveillance or fire control functions.


Situational Awareness:
Driver Vision Enhancer:The Tiger features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 12 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The Tiger is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted to the turret roof each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions. Each STAS module also contains an imaging sensor autoprocessor (ISA) similar to the one in the gunner and commander FLIR sights which provides automatic target recognition (ATR) capability of threats detected by the system. The STAS can be used to monitor the area around the vehicle during silent watch or while the crew is asleep and includes automatic alert broadcast and target-tracking/moving-target indicator functions which can track detected threats and can interface with the fire control system to hand-off threats to the gunner or commander's sight for immediate engagement by the tank's main or coaxial armament.

Vehicle Missile & Laser Warning Receiver: The vehicle comes equipped with a missile and laser warning system derived from SDI's SN/AAR-64 airborne Missile/Laser Warning System which provides passive warning of incoming threat missiles and illumination by threat lasers. The system employs four optical sensor heads with integral optical signal converters placed around the turret of the vehicle with 360 ° azimuth and -10° to + 45° elevation coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which detects lasers in the 0.4-2.1 μm and 8-12 µm wavelength range including laser designators, illuminators, and rangefinders, and a short-wave infrared (SWIR) camera which provides muzzle flash detection detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays and features integral counterfire capability where the system can automatically slew the turret to within <2 degrees RMS of detected laser or missile threats through a button on the vehicle commander's joystick, presenting the frontal armor of the turret towards the threat and allowing the threat to be rapidly engaged by the tank's armament.

Vehicle Radar Warning Receiver: In addition to the missile and laser warning system the vehicle is fitted with radar warning receivers which warn the crew when the vehicle is being illuminated by a ground or airborne based radar system. The RWR system employs four circularly polarized spiral antennas co-located with the missile/laser warning receiver sensors which provide 360° azimuth and -5° to + 80° elevation detection of RF signals in the 2-40 GHz range. The four antenna feed into two identical receiver connected to a common processor and control unit inside the vehicle. An alphanumeric display and an interface to the vehicle's intercom system provides both visual and audio warning to the crew when the vehicle is being illuminated by a radar including radar type, direction, and scan mode. Like the RWR system is integrated into the vehicle's fire control system and features counterfire capability which automatically slew the turret to within <2 degrees RMS of detected threats through a button on the vehicle commander's joystick.

Acoustic Gunshot Location System: The turret of the vehicle is fitted with an SDI acoustic gunshot location system (AGLS) which uses a series of microphones to triangulate the location of incoming small arms, cannon, and rocket fire. The AGLS uses an array of four microphones fitted to a mast mounted to the rear of the turret which provides 360° hemispherical coverage around the vehicle. Incoming fire is triangulated to a probable shooter location with +/- 2° azimuth, +/-3° elevation, and +/- 10% range RMS error with the ability to interface with the vehicle's GPS system to provide 10 digit grid coordinates of the shooter probable location. The AGLS also interfaces with the vehicle's fire control system and can automatically slew the turret or RWS in the direction of detected threats.


Communications:
Vehicle Multiband Networking Radio: The primary radio system of the vehicle is an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.


Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network.


AI Modules:
To aid in the performance of the crew the PzKpfw 151 Tiger vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, C3 (command, control, and communications), and target acquisition and engagement which provide automatic communication management, sensor control, and target identification and tracking,

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.

Target Acquisition & Engagement (TA&E): The Target Acquisition & Engagement or TA&E module is responsible for generating and updating track files of enemy contacts and disseminating them to the other AI modules and advising the vehicle commander on recommended actions in repose to enemy contacts. The TA&E module takes input from the dual band FLIR and TV cameras and the laser rangefinders in the gunner and commander sights and generates track reports of each contact including type (tank, helicopter, APC), position (GPS grid coordinates and elevation), heading (degrees), moving (yes/no), activity, and sensors used. Different vehicle sensors are used to fill out the different parts of the contact report, ie the automatic target recognition (ATR) capability of the dual band FLIR sights are used for determining contact type while the laser rangefinder and far target locator (FTL) system are used to fill in contact position and heading. After a track report has been generated the module then determines the kill probability (the probability the own vehicle can successfully engage and defeat the contact with its own weapons) and the contact danger (the probability the contact will detect and engage the own vehicle) based on contact type and position, own vehicle position, and environmental factors including terrain and ambient weather conditions. Contact danger will also be judged as extreme if the vehicle's missile, laser, and radar warning sensors indicate the tank is being actively illuminated or shot at. In response to extreme danger contacts the module will automatically deploy smoke grenades in the threat direction and prompt the crew to immediately move and engage the threat with the vehicle's weaponry. If the contact threat is judged as less severe the module can run various simulations to evaluate possible engagement scenarios and provide a recommended engagement option which could be to engage the contact with the vehicles weapons, continue monitoring the contact with the vehicle's sensors, or to simply ignore it.
Last edited by The Technocratic Syndicalists on Thu Feb 15, 2024 10:27 am, edited 171 times in total.
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Postby The Technocratic Syndicalists » Sat Jun 03, 2017 9:46 pm

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IfKpfw 501 Goliath

General Characteristics:
  • Type: Infantry fighting vehicle
  • Weight: 62.3 t
  • Length: 7.9 m
  • Width (hull): 3.7 m
  • Height: 3.0 m
  • Crew: 3 (driver, gunner, commander) + 8 dismounts

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,760 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,200 l
  • Operational range: 550 km

Armament:
  • 1x MK50 50 mm chain gun, 300 rounds
  • 2x twin-tube ATGM launchers, 8x RBS 94 Lance Hypervelocity ATGMs
  • 1x 8 mm MG 45E, 2,000 rounds
  • 1x 40mm GMG 97, 240 rounds
  • 4x 71mm flare mortars, 12 rounds

Maneuverability:
  • Power/weight Ratio: 35.5 PS/t (25.8 kW/t)
  • Ground clearance: 0.55 m
  • Gradient: 70%
  • Sideslope: 40%
  • Fording depth: 1.2 m
  • Trench crossing: 2.5 m
  • Vertical wall climb: 1.0 m


Overview
The Infanteriekampfwagen 501 (IfKpfw 501) Goliath is a heavy infantry fighting vehicle (HIFV) designed by SDI Vehicle Systems. The Goliath features armor protection comparable with modern main battle tanks combined powerful autocannon and anti-tank missile armament and the ability so seat 8 infantry dismounts. Although not a common chassis the Golitah shares its engine, transmission, and running gear with SDI's PzKfz 151 Tiger main battle tank, easing logistics for units equipped with both vehicles


Armament
SDI MK50 Cannon
  • Type: Chain gun
  • Weight: 520 kg
  • Length: 4,700 mm
  • Barrel Length: 4,150 mm
  • Width: 450 mm
  • Height: 320 mm
  • Caliber: 50 x 330 mm
  • Rate of fire: Single shot or variable 150-400 RPM
  • Power requirement: 6 kW
BGM-194 Lance
  • Type: Hypervelocity ATGM
  • Length: 1,500 mm
  • Diameter: 150 mm
  • Weight: 50 kg
  • Speed: 2,400 m/s
  • Range: 10 km
  • Propulsion: dual-pulse solid-fuel rocket
  • Warhead: 5 kg DU alloy penetrator

Cannon Armament: The primary armament of the Goliath is the SDI MK50, a 50mm caliber electrically driven linkless dual-feed automatic cannon which is located in an unmanned, fully stabilized turret at the rear of the vehicle. The turret uses electric turret drives and can traverse a full 360º at up to 45°/s and elevate from -10º to +45º at 45°/s with < 0.3 mrad pointing accuracy in both traverse and elevations. The MK50 is an electrically powered chain-gun weapon firing from an open-bolt with a linkless dual-feed ammunition system. Power for the cannon is provided by an 8 kilowatt brushless DC motor which allows for a selectable rate of fire between 150 and 400 rounds per minute. Empty cases are ejected forward through two ejection chutes located underneath and on either side of the barrel. Both the barrel and receiver are chrome-lined for improved service life. An additional rectangular stiffening sleeve with cooling vent cutouts is attached to the barrel to improve accuracy during fully automatic fire on the high rate-of-fire setting. 150 rounds of 50 x 330 mm ammunition are stored ready to use in the turret in two 75 round boxes with another 150 50mm rounds stowed inside the hull. For firing programmable air-burst munition rounds the 50mm cannon features a muzzle programming unit containing magnetic flux sensor coils which measures the muzzle velocity of each round leaving the barrel and programs the round to explode in-flight after a set distance. Standard ammunition is either 50x330mm APFSDS-T (Armor piercing discarding sabot w/ tracer), an armor-piercing round employing a depleted uranium staballoy penetrator capable of penetrating in excess of 180 mm RHA at 1,500 meters, and PABM-T (Programmable airbust munition w/ tracer), a HE-fragmentation round with a programmable fuze which can be set to various airburst, impact, or delay settings.

Secondary Armament: An 8mm MG 45E machine gun is mounted coaxial to the main armament with 1,000 rounds stored ready to fire in the turret and another 1,000 rounds stored in the hull. The turret of the vehicle additionally includes an SDI GMG 97 40mm grenade-machine gun (GMG) mounted to a remote weapon station attached to commander's sight on top of the turret. The SDI GMG 97 is short-recoil operated, belt fed automatic grenade launcher capable of firing high velocity 40mm programmable air-burst grenades out to an effective range of 1,500 meters. The weapon station includes a box containing a 48 round belt ready to fire with another 192 rounds of 40mm ammunition stored in the hull.

Missile Armament: To combat main-battle tanks and other heavy vehicle threats the Goliath is equipped with twin turret mounted missile launchers containing two RBS 94 Lance missiles each. The RBS 94 Lance is a hyper-velocity anti-tank guided missile (HVATGM) which features a dual-pulse solid fuel rocket which accelerates the missile at over 1,000 gs to to a burnout velocity of over mach 6 at sea level. The missile employs side-scatter laser beam riding guidance system which uses the vehicle's FLIR and 1.06-μm laser designator to deliver guidance updates to the missile in flight. In addition to the four missiles stored ready to fire in the turret the vehicle carries another four missiles in the hull as reloads.

Smoke-grenade launchers: The vehicle is equipped with a total 16 smoke grenade launchers grouped into two sets of 4-tube launchers on either side of the turret face which cover the forward two 90º sectors. The smoke launchers fire 76 mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual (0.4 to 0.7 µm) and infrared (0.7 to 14 µm) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. Each smoke grenade weighs 1.2 kg including 800 grams of red phosphorous fill and is launched to a range of 40-45 meters where the grenade bursts and produces a smokescreen approximately 12 meters long and 6 meters high for a duration of 20-30 seconds. The launchers can also fire fragmentation grenades containing an explosive charge and 750 grams of steel balls which are designed to burst at a height of 5-6 meters above the ground. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each 90° sector.

Flare mortars: Mounted to the turret of the vehicle are four 71 mm flare mortars which are designed to fire infrared flares designed to provide near-infrared wavelength illumination of target areas at night or during low-visibility weather conditions for dismounted infantry units equipped with night vision goggles. The four flare mortars are divided into two groups of two mortars each with each pair having a control unit with firing buttons inside the crew compartment and a connection cable which is connected to the vehicle's 24V DC electrical bus. Each mortar has a fiberglass barrel approximately 91 centimeters long and fires a 34 centimeter long flare massing 1.2 kg at a muzzle velocity of around 147 m/s. The barrel can be elevated from 0°to +45° in 5° steps with the launcher having three preset ranges of 450, 950, and 1,600 meters. Each flare consists of a front segment containing an electrical time fuse, pyrotechnic charge, separating charge and infrared spectral flare, rear segment with a parachute, and a tail section which contains stabilization fins and the propellant charge. The time fuze triggers the separating charge which causes the munitions front and rear segments to split and release the infrared flare along with the parachute assembly which is ejected by a spring in the rear projectile segment. The flare then ignites and burns for around 30 seconds as it descends towards the ground at a rate of around 3 m/s. The flare provides illumination in the 0.7-1.2 µm region and illuminates a ground area around 1,500 meters in diameter. Four flares are carried in the four turret mounted mortars with another eight normally stored inside the crew compartment.


Protection:
Armor protection:The hull of the vehicle is equipped with a multi-layer composite armor scheme designed to protect the vehicle from both tank cannon fired kinetic energy penetrators and large-caliber anti-tank guided missile threats. The composite armor employs multiple layers of plastic, ceramic, and metal alloys and is designed to stop 120 and 125 mm APFSDS ammunition (800-900 mm RHA penetration) and 170 mm diameter HEAT warheads (up to 1500 mm RHA penetration) across the frontal 60° and 40mm APFSDS ammunition (up to 200 mm RHA penetration) and 110 mm diameter HEAT warheads (up to 900 mm RHA penetration) across the frontal 180°. The vehicle's remote turret is substantially less armored than the hull and consists of welded 7039 aluminum alloy plates covered with ceramic/elastomer composite armor panels which provides the remote turret with 360° protection against 15mm AP ammunition and 155mm shell fragments. The roof of the hull and turret features an additional layer of composite armor designed to defeat bomblets and top-attack EFP submunitions and is designed to stop shaped charge warheads up to 70 mm in diameter and EFP warheads up to 150 mm in diameter. The vehicles side armor is also augmented by a total of 88 heavy explosive reactive armor (ERA) modules embedded to the vehicle's side skirts which provide additional protection against large diameter shaped charge and tank gun fired APFSDS ammunition. Each ERA module employs a metal-free composite construction and contains two reactive layers and a passive layer consisting of ceramic composite plates sandwiching an explosive or inert elastomer layer (respectively). Minimization of post-armor effects of both kinetic energy projectiles and shaped charge warheads is achieved through the use of flexible spall panels which are fitted to the inside surfaces of the vehicle. The spall liner employs multiple layers of orthogonally cross-plied M5 ballistic fibers which are pressed together into a single layer which is then laminated into a flexible thermoplastic resin. The liner serves to reduce the spall cone angle of spall fragments, reducing the spread of fragments inside the vehicle and thus minimizing the chances that a penetrating round will injure or kill the crew.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80° C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously online begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: The Goliath is equipped with SDI's Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT and APFSDS projectiles. The system consists of a set of pre-warner radar arrays and multiple hybrid protection modules mounted along the front, sides, and rear of the hull consisting of embedded electro-optical tracking sensors and directional explosive countermeasures which are encased in a layer of ceramic armor which provides protection for the system components and acts as additional passive armor for the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels mounted around the vehicle on the outside of the APS modules which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) tungsten-nickel-cobalt (WNiCo) alloy shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the hull to have overlapping coverage over the the entire hull of the vehicle by steering the blast side to side and downwards or to defeat over-fly top attack munitions by steering the blast upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past 4 or so meters from the vehicle. To protect the APS modules from shell fragments, small arms fire, and other sources of damage and to absord the residual debris from projectiles intercepted by the system the sensors and explosive countermeasure are encased in a layer of encapsulated ceramic armor rated to stop 14.5mm AP at 20 meters and 152/155 mm high explosive shell fragments at 30 meters. The system is capable of intercepting four simultaneous threats and with a reaction time of 0.5 milliseconds is capable of intercepting RPGs or other munitions launched from within 10 meters of the vehicle.


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Goliath is powered by a self contained front drive system separated from the fighting compartment by a fireproof bulkhead which includes an AMG (Arkaenisch Motorenfabrik Gesellschaft) designed HL280 diesel engine and AMG AK 7-700 hydro-kinetic planetary transmission, accessory drive gearbox, auxiliary power unit (APU), self-cleaning air filter (SCAF), exhaust IR suppression system, engine and APU fuel system, and the vehicle electrical system. Inlet air for the engine flows through a set of armored grills located on front of the hull before being scrubbed by a pre-cleaner and passed through a self-cleaning air filter (SCAF) where the now cleaned air then enters the engine. The exhaust from the engine is passed through an IR suppression system and then finally vented overboard through a louvered grill mounted at the front of the vehicle. Relatively compact and designed for reliability and ease of maintenance, the vehicle's power pack has a 5,000 hour mean time between overhaul (MTBO) and air filters designed for 100 hour continuous operation at twice zero-visibility dust concentrations, can accept virtually any grade of diesel or jet fuel, can cold start at temperatures as low as -50º C, and can be removed from the vehicle in as little as 15 minutes for replacement or repair.

Engine: The AMG HL280 diesel engine is a multi-fuel, low-heat rejection (LHR), quad-turbo diesel engine with a maximum power output of 1,765 kilowatts (2,400 PS) at its maximum rated speed of 3,300 RPM. The HL280 engine block is a monobloc design with a 60º cylinder bank angle and is constructed from compacted graphite iron (CGI) and features integral charge air cooler and intake manifold housings along with machined cooling passages for the synthetic oil coolant. Both the turbocharger intercooler and aftercoolers and exhaust manifolds are constructed from high-temperature stainless steel alloy and are located on the outside of the V-block with the intake manifolds integral to the V-block itself. The HL280 features a common rail electronic controlled injection (ECI) system with one piezoelectric injector per engine cylinder. Fuel is pressurized by a high-pressure, fuel lubricated hydraulic boost pump with the fuel rail mounted on the engine serving as a high-pressure accumulator. The fuel is distributed to the individual fast-switching piezoelectric injectors integrated into each engine cylinder where fuel is then injected at 2,500 bar pressure into each engine cylinder. The cylinder heads are constructed from cast ductile iron and feature black nitride coated stainless steel inlet valves and high temperature titanium/inconel alloy exhaust valves with monolithic zirconia valve seats capable of surviving the high exhaust gas temperatures of each cylinder without needing cooling. The piston in each cylinder is two piece, articulated design with a forged maraging steel crown with tungsten-carbide piston rings screwed into an aluminum skirt assembly, the steel crown of the piston cooled using a single piston oil supply nozzle located on the underside the crown. Both the cylinder head and piston crown feature a plasma-spray applied 2mm zirconia ceramic thermal barrier coating (TBC) which facilitates high temperature, high pressure engine operation with minimal thermal losses. The cylinders themselves are constructed from ductile cast iron with an aluminum-silicon carbide metal matrix composite liner with an diamond-like carbon (DLC) coating which reduces both the head temperature and the friction between the piston rings and the cylinder walls. The cylinders are cooled using synthetic oil which flows through an annular groove at the top of the cylinder in between the cylinder block and cylinder liner. The engine's crankshaft and connecting rods use an induction hardened, forged maraging steel alloy construction with diamond-like carbon (DLC) coatings to improve abrasion and corrosion resistance. The connecting rods are a telescoping design which allows for the compression ratio of the engine to be varied from 9 up to 18, allowing for the cycle isotropic efficiency to be maximized across the engine's entire operating envelope. The intake pressure of the HL280 engine is boosted via the use of four variable-geometry sequential turbochargers. The turbine of each turbocharger is a single, stage axial design constructed from silicon nitride ceramic and features a set of axially pivoting variable-area turbine vanes which open up at low engine RPMs to reduce turbo-lag and increase engine torque and then at higher engine RPMs close down to increase engine boost pressure. The exhaust turbine of each turbocharger drives both a low pressure compressor (LPC) and high pressure compressor (HPC) on a common shaft with an air-oil intercooler placed between the low pressure and high pressure stages and an air-oil aftercooler placed after the high-pressure stage of each turbocharger. Each turbocharger additionally features set of variable inlet guide vanes (VIGVs) ahead of low and high pressure compressors which prevent surge or chocking of the flow through the compressor.

Transmission: The transmission used with the HL280 engine is the AMG AK 7-700 hydro-kinetic power shifting, reversing, and steering transmission with seven forward and three reverse gears. The transmission employs a powershift system with planetary gearing capable of shifting under full engine load, a reversing gear mechanism, and a hydrokinetic torque converter with a lock-up clutch to improve efficiency at higher speeds. Operation of the transmission is fully automatic and automatically changes gear within a range pre-selected by the driver. A digital transmission control unit (TCU) is used to control shifting in automatic mode which interfaces with the engine control unit (ECU) to control the range of the transmission. A manual override is additionally fitted which allows for range override of the transmission through a lever in the driver's compartment connected through a cable to a series of mechanical linkages attached to the shifting mechanism of the transmission. The steering drive fitted to the transmission is an infinitely variable hydrostatic/hydrodynamic superimposed differential system employing twin hydraulic drives with variable-displacement hydraulic pumps and twin hydraulic motors which are used to add or subtract power from each side of the vehicle and allow for neutral or pivot turning at infinitely variable speed. Braking functions of the transmission include a combined hydrodynamic/mechanical dual circuit integrated brake system with an internal hydrodynamic brake and external oil-cooled power assisted disc brakes on either side of the transmission. Independent service and parking brakes are additionally included. A hydraulic power take-off (PTO) system fitted to the transmission output is used to power the transmission cooling fans as well the accessory drive gearbox which contains a toroidal CVT (continuously variable transmission) which provides a constant 3,000 rpm speed output independent of engine RPM which is used to drive the vehicle's NBC compressor, alternator, self-cleaning air filter (SCAF), scavenge blower, and IR exhaust suppression system.

Auxiliary Power Unit: Auxiliary power is provided via an SDI RKM700 under-armor auxiliary power unit (APU) attached to the accessory gearbox within the engine compartment. The APU system consists of the RKM700 engine along with integral starter, fuel conditioning system, and self-contained cooling system and is used to power the vehicle's alternator, air filter compressor, and self-cleaning air filter while the engine is offline. The RKM700 APU is a single-cylinder turbocharged rotary engine with a 0.7 liter displacement which can generate a maximum of 60 kilowatts (80 PS) of power at it's rated speed of 6,000 RPM. In addition to the single-stage turbocharger the RKM700 engine features an air-to-air aftercooler and a dry-sump oil lubrication system. The RKM700 APU is oil-cooled using an integral oil-air heat exchanger and cooling fan. The APU is fed from the main engine air inlet and exhausts though a grille in the upper left hull sponson.

Electrical System: The vehicle's electrical system interfaces with the engine and transmission, CVT accessory drive gearbox, self-cleaning air filter (SCAF,) APU, NBC filtration system, HVAC system, fuel system, and fire suppression system. The electrical system is consists of four 170 amp-hour lithium-ion batteries, battery heater system, electrical distribution system, and a 1,000 amp, 28 kilowatt oil-cooled brushless permanent magnet alternator driven by the APU or main engine through the CVT accessory drive gearbox. The lithium-ion batteries are wired in series-parallel and provide 680 amp-hours capacity of 24 VDC output from -40 degrees to +50 degrees C ambient temperature and allow for engine cold start at -40º C without the APU after up to four hours of silent watch. The batteries are charged using the 1,000 amp oil-cooled alternator through a solid-state voltage regulator which at an alternator speed of 3,000 rpm delivers 28-30 volts of DC power at up to 150 amps to rapidly charge the batteries.

Suspension & Running Gear: The Goliath features a fully decoupled running gear where the road wheels, suspension arms, idlers, sprockets, and final drivers are mounted on left and right running gear carriers which are decoupled from the hull sides using a series of shock-absorbing elastomer mounts which substantially reduces the structural vibration and noise of the running gear elements. The lack of penetration of running gear elements into the hull also significant improves the mine protection of the vehicle. The vehicle's fuel tanks are additionally enclosed within the external running gear carriers which reduces the chance of a fuel fire spreading into the crew compartment if the fuel tanks are penetrated. The suspension system used by the Goliath is an SDI designed semi-active in-arm hydro-pneumatic suspension system with four sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (16 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The suspension also allows the vehicle to "tilt" forwards or backwards permitting additional gun elevation and depression. The vehicle employs SDI designed double-pin, twin center guide tracks with removable rubber road-pads. Track width is 75 centimeters with a pitch of 20 centimeters with a total of 88 links per track. To reduce weight the track links and pins employ a novel composite construction using a particle reinforced titanium metal matrix composite in place of traditional steel. The track parts are formed through powder metallurgy using titanium carbide (TiC) particles mixed into Ti-6Al-6V-2Sn (Ti-6-6-2) alloy powder, the final composite parts offering superior corrosion and wear resistance to steel parts while reducing track weight approximately 25% over an equivalent strength steel design. Each track link is fitted standard with twin detachable road pads constructed from a kevlar-rubber composite to reduce noise and road wear. The vehicle's sixteen road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units.


Fire Control:
Gunner's Sight: The vehicle is equipped with an SDI two-axis stabilized gunner's thermal sight which is housed on the left side of the vehicle's remote turret. The main features of the sight are a third generation dual-wavelength (3-5 um and 8-14 um) thermal imager and high-resolution color CCD imager with 2-axis independently stabilized line of sight, ballistic computer, eye-safe laser rangefinder, and integrated GPS/inertial navigation system. The sight is encased within an armored housing rated to stop 14.5mm AP at 20 meters and 152/155 mm high explosive shell fragments at 30 meters and can be traversed +/- 7.5° in azimuth and elevated from -13° to +45° in elevation. The entire sensor head can also be rotated back 180 ° to shield the optics from damage. The third generation thermal imager used with the gunner's sight is SDI's WBG-3G, a1280 x 1024 pixel dual color (MWIR and LWIR) capable Mercury cadmium telluride (HgCdTe) staring focal plane array (FPA) detector based system which features an architecture common to several other SDI designed third gen thermal imaging systems. The thermal imager is cooled using a Stirling cycle linear drive cryocooler which cools the detector assembly to 77°K. The detector and crycooler system are contained in a single Standard Advanced Dewar Assembly (SADA), a closed-cycle dewar-cooler assembly containing the linear crycooler, infrared FPA, Dewar, and various control electronics and sensors. The dual-color thermal imager features a color fusion system which assigns colors to pixel values from each MWIR and LWIR band (red for LWIR, cyan for MWIR), adding color contrast to the otherwise black-and-white thermal image. The thermal sight can be toggled between 16.7° wide field of view (WFOV), 8.9° medium field of view (MFOV), 4.4° narrow field-of view (NFOV), and 2.2° ultra-narrow field of view settings. Mounted alongside the thermal imager is a 1920 x 1080 pixel visible/near IR monochrome CCD camera with selectable 16.7° wide field of view (WFOV), 8.9° medium field of view (MFOV), 4.4° narrow field-of view (NFOV), and 2.2° ultra-narrow field of view settings which provides the gunner's sight with an additional daylight channel in addition to the dual-band thermal channel. Detection, recognition, and identification ranges for the sight are around 17/9/5 km for the thermal channel and 18/8.5/4.5 km for the daylight channel against a 2.3 x 2.3 meter vehicle target. An image fusion function is also available combines the data from the dual-band thermal imager and the CCD camera to provide a fused image selectable on the sight control panel from 100% visible / 0% IR to 0% visible / 100% IR in infinitely variable increments. Range information for the fire-control system is provided by a 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder which provides range data accurate to 1 meter from ranges of 80 meters up to 20 kilometers. The sight additionally contains a 1.064 um laser designator, laser illuminator and laser spot tracker. The sight's dual axis stabilized head mirror assembly provides for enhanced on-the-move (OTM) stabilization capability, ensuring the reticle of the sight stays stabilized in the center of the sight while the vehicle is on the move. Dual-axis stabilization is provided by micromachined 2-axis hemispherical Resonator Gyroscopes (HRGs) with 0.001 °/hour drift capability integrated into the sights inertial measurement unit (IMU) system. The output from the sight is displayed in the gunner's binocular image control unit (BICU), a dual binocular display mounted in the gunner's station which generates a stabilized virtual image of the output of the sighting unit.

The gunner's sight is further integrated with a GPS/INS navigation system which inputs accurate heading, attitude, velocity and position information of the vehicle into the sight's ballistic computer. The navigation system combines 3 axis fiber optic gyroscopes, 3 axis pendulous accelerometers, and digital magnetic compass with further sensor input from vehicle motion sensor (VMS) systems in the drivetrain and two lightweight, jam resistant DGPS antenna integrated into either side of the sight housing. Attitude information from the GPS is used to give the sight far target location (FTL) capability which combines data from the GPS/INS system and laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The ballistic computer takes into account the target range, vehicle cant angle, the direction of vehicle motion relative to the target, crosswind velocity and direction, and the ballistic data of the selected ammunition in order to calculate the required lead and elevation to hit the target. The firing solution is then automatically transferred to the turret's stabilization and control system which then lays the turret onto the line-of-sight of the gunner's sight. The gunner's sight also features an automatic target recognition (ATR) capability imaging through an SDI designed imaging sensor autoprocessor (ISA) unit built into each sight. The ISA employs parallel very high speed integrated circuit (VHSIC) processors operating at 10 billions of operations per seconds (BOPS) contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the sight's dual-band FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, and other armored vehicles.

Commander's Sight: External vision for the commander is provided by a stabilized panoramic commander sight which features the same infrared imager, CCD camera, laser range finder, and other optics as the gunner's sight. The commander's sight features independent dual-axis HRG stabilization along with servomotor actuated 360° azimuth and -17° to +45°elevation travel and < 0.5 mrad stabilization accuracy. Like the gunner's sight the commander's sight is contained within an armored housing which protects the assembly against shrapnel and small arms fire. The commander's sight includes track-while-scan capability and an integral ballistic computer and ATR processor identical to the one in the gunner's sight which enables lead angle computation capability and far-target location ability like that of the gunner's sight. The commander's sight features both manual and automatic scan settings and an additional gun line of sight (GLOS) mode where the remote turret is slaved to the commander's sight, allowing the commander to aim and fire the vehicle's cannon and missile armament. High definition video output from the commander's sight is transferred into the turret via a 100 MHz bandwidth fiber-optical slip ring and displayed on the commander's integrated display (CID), a 1920 x 1080 resolution touchscreen SXGA display with 20 programmable edge keys all with variable backlight which can each be assigned to various surveillance or fire control functions.


Situational Awareness:
Driver Vision Enhancer: The vehicle features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 14 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55 x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: For enhanced situational warns the vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted on the corners of the hull each containing two 640×480 pixel long-wave infrared (8-14µm) thermal imagers and two ultra-high resolution color CMOS daylight CCD cameras set a 90°angle from each other. The four sensor modules provide overlapping 360 degree horizontal field-of-view and -30° to +45°vertical field-of-view day and night vision around the vehicle The STAS is capable of detecting a person sized target out to 300 meters (900 meters with the daylight channel) and includes automatic alert broadcast and target-tracking/moving-target indicator functions and can interface with the fire control system to hand-off threats to the gunner or commander's sight for immediate engagement by the tank's main or coaxial armament.

Missile/Laser Warning System: The vehicle is equipped with a passive missile and laser warning system which provides both warning of incoming threat missiles and illumination by threat lasers. The system employs five optical sensor heads with integral optical signal converters mounted around the turret which provide combined 360° azimuth coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which warns the crew when the vehicle is being illuminated by a laser designator/illuminator/rangefinder or if the aircraft is being targeted by a laser beam-riding missile, and a short-wave infrared (SWIR) camera which provide detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays. The system is also integrated into the vehicle's fire control system and features integral counterfire capability where the system can automatically slew the turret to within <2° RMS of detected laser or missile threats through a button on the vehicle commander's joystick to allow the threat to be rapidly engaged by the vehicle's armament.

Vehicle Radar Warning Receiver: In addition to the missile and laser warning system the vehicle is fitted with radar warning receivers which warn the crew when the vehicle is being illuminated by a ground or airborne based radar system. The RWR system employs four circularly polarized spiral antennas co-located with the missile/laser warning receiver sensors which provide 360° azimuth and -5° to + 80° elevation detection of RF signals in the 2-40 GHz range. The four antenna feed into two identical receiver connected to a common processor and control unit inside the vehicle. An alphanumeric display and an interface to the vehicle's intercom system provides both visual and audio warning to the crew when the vehicle is being illuminated by a radar including radar type, direction, and scan mode. Like the RWR system is integrated into the vehicle's fire control system and features counterfire capability which automatically slew the turret to within <2 degrees RMS of detected threats through a button on the vehicle commander's joystick.

Acoustic Gunshot Location System: The turret of the vehicle is fitted with an SDI acoustic gunshot location system (AGLS) which uses a series of microphones to triangulate the location of incoming small arms, cannon, and rocket fire. The AGLS uses an array of four microphones fitted to a mast mounted to the rear of the turret which provides 360° hemispherical coverage around the vehicle. Incoming fire is triangulated to a probable shooter location with +/- 2° azimuth, +/-3° elevation, and +/- 10% range RMS error with the ability to interface with the vehicle's GPS system to provide 10 digit grid coordinates of the shooter probable location. The AGLS also interfaces with the vehicle's fire control system and can automatically slew the turret or RWS in the direction of detected threats.


Navigation & Communications:
Hybrid Navigation System: The primary navigation sensor of the vehicle is an SDI TNS 2000 tactical hybrid navigation system which consists of a 6-axis IMU coupled to a 24 channel dual-frequency (L1/L2) SAASM (Selective Availability Anti-spoofing Module) based GPS receiver. The IMU is coupled to the vehicle's VMS (vehicle motion sensor) system and consists of a three Axis ring laser gyroscope (RLG) and provides <0.7% distance travelled horizontal position accuracy, <0.4 % DT distance travelled altitude accuracy and <0.015 ° pitch and roll determination for the vehicle's fire control system. With GPS the system has <6 meter horizontal position and <10 meter attitude determination accuracy with <0.3° RMS heading/pointing accuracy. The system provides continuous position and heading data and ne aligned either while stationary or while moving with a <20 minute static and <16 minute dynamic maximum alignment time.

On the move SATCOM: To support secure, high bandwidth, over-the-horizon transmission of voice, video and sensor data the turret of the vehicle is fitted with an SDI Ka-band (30 – 31 GHz transmit and 20.2 – 21.2 GHz receive) SATCOM on-the-move (SOTM) antenna system designed to maintain satellite connectivity as the vehicle driving across rough terrain and at vehicle speeds of up to 100 kilometres per hour. The antenna features dual circular polarization and is mounted to a servomotor controlled two-axis stabilized gimbal with the ability to steer 360° azimuth and 0°to +95° in elevation. The antenna is designed to to transmit with up to 13 Watts of power with 1 GHz of instantaneous bandwidth and is contained inside a 46 centimeter diameter fiber/resin ballistic radome mounted to the roof of the turret.

Vehicle Multiband Networking Radio:In addition to the SATCOM the vehicle is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use time-division multiple access (TDMA) networking waveforming and supports inter-battalion and inter-brigade self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simultaneous nodes with transmit speeds of up to 8 Mbps.


Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network.


AI Modules:
To aid in the performance of the crew the IfKpfw 501 vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, C3 (command, control, and communications), and target acquisition and engagement which provide automatic communication management, sensor control, and target identification and tracking,

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. For example if the system receives an track report than an enemy vehicle(s) are moving along a road it will assume that the vehicle(s) have not detected the presence of own or friendly forces and will keep moving down the road. On the other hand if another track report is received indicating that the enemy vehicle(s) have moved off-road and actively engaging with their armament the system will assume that own or friendly forces have been detected and that the targets will attempt to retreat and form a defilade position. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.

Target Acquisition & Engagement (TA&E): The Target Acquisition & Engagement or TA&E module is responsible for generating and updating track files of enemy contacts and disseminating them to the other AI modules and advising the vehicle commander on recommended actions in repose to enemy contacts. The TA&E module takes input from the dual band FLIR and TV cameras and the laser rangefinders in the gunner and commander sights and generates track reports of each contact including type (tank, helicopter, APC), position (GPS grid coordinates and elevation), heading (degrees), moving (yes/no), activity, and sensors used. Different vehicle sensors are used to fill out the different parts of the contact report, ie the automatic target recognition (ATR) capability of the dual band FLIR sights are used for determining contact type while the laser rangefinder and far target locator (FTL) system are used to fill in contact position and heading. After a track report has been generated the module then determines the kill probability (the probability the own vehicle can successfully engage and defeat the contact with its own weapons) and the contact danger (the probability the contact will detect and engage the own vehicle) based on contact type and position, own vehicle position, and environmental factors including terrain and ambient weather conditions. For example if an enemy tank is detected at 2,000 meters while the own vehicle is moving in open terrain the contact danger will be judged as extreme while if the same tank is detected while the own vehicle is an a stationary hull-down or defilade position the contact danger will be judged as less severe. Contact danger will also be judged as extreme if the vehicle's missile, laser, and radar warning sensors indicate the tank is being actively illuminated or shot at. In response to extreme danger contacts the module will automatically deploy smoke grenades in the threat direction and prompt the crew to immediately move and engage the threat with the vehicle's weaponry. If the contact threat is judged as less severe the module can run various simulations to evaluate possible engagement scenarios and provide a recommended engagement option which could be to engage the contact with the vehicles weapons, continue monitoring the contact with the vehicle's sensors, or to simply ignore it.
Last edited by The Technocratic Syndicalists on Wed Nov 16, 2022 8:26 am, edited 82 times in total.
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Founded: May 27, 2015
Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Sat Nov 03, 2018 7:26 pm

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PzH 173 Chimera

General Characteristics:
  • Type: Self Propelled Howitzer
  • Weight: 60.0 t
  • Length (hull): 7.9 m
  • Length (gun forwards): 15.2 m
  • Width: 3.8 m
  • Height: 2.8 m
  • Crew: 3 (driver, gunner, commander)

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,300 l (340 Gallon)
  • Operational range: 550 km

Armament:
  • 1x 17 cm L/60 Artillery Gun, 40 rounds
  • 1x 8 mm MG 45E, 2000 rounds

Maneuverability:
  • Power/weight Ratio: 40.0 PS/t (29.4 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.90 kg/cm2
  • Gradient: 70%
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
The Panzerhaubitze 173 (PzH 173) Chimera is an armored, tracked self-propelled howitzer designed by SDI Vehicle Systems. The vehicle consists of an unmanned turret housing a 17 cm cannon, ammunition, and autoloader mechanism mated to a hull based on a modified PzKfz 151 Tiger chassis with common powerpack, suspension, and running gear. A complete Chimera artillery system includes a PzH 173 self propelled howitzer and a MtPzA 173 (Munitionstransportpanzer - Artillerie 173) resupply vehicle which reloads and fuels the self propelled howitzer using an automated robotic handling system.


Armament
SDI 17 cm L/60 Artillery Gun:
  • Bore diameter: 172.5 mm/i]
  • Barrel length: [i]1,035 cm
  • Overall length: 1,087 cm
  • Tube weight: 4,650 kg
  • Overall weight: 5,300 kg
  • Chamber volume: 47.5 l
  • Projectiles: SDI 17 cm series
  • Charges: SDI AM95 bi-modular charge system, Zones 1-7
  • Muzzle Velocity: 1,050 m/s (AM90 zone 6)
  • Chamber Pressure: 430 MPa (AM90 zone 6)
  • Range Hollow Base (HB): 48 km (AM90 zone 6)
  • Range Base Bleed (BB): 65 km (AM90 zone 6)
  • Range Base-Bleed/Rocket Assist (BB/RA): 85 km (AM90 zone 6)
The vehicle's main armament is The SDI 17 cm L/60 Artillery Gun, a 17 cm liquid cooled, autoloading howitzer which is contained in an unmanned turret located in the center of the vehicle. The complete armament system comprises the gun tube assembly, a wedge breech block assembly, recoil and recuperator system, ballistic protection, elevating mechanism interface, midwall liquid cooling system, and temperature sensors for thermal management. The barrel has a length of 60 calibers and uses a two-piece construction with an inner autofrettaged steel liner and an outer composite jacket consisting of carbon fibers transversely wound into a high-modulus polyetheretherketone (PEEK) matrix which is wrapped over the inner pre-stressed steel liner . The rifling consists of 48 grooves with a uniform right-hand twist with a 1:20 twist rate. The gun barrel and breach are plated with an explosively bonded tantalum alloy refractory liner for increased barrel life. The end of the barrel also includes an slotted, multi-baffle muzzle brake to reduce recoil force. The recoil system is a conventional hydropneumatic recuperator mechanism with two recoil cylinders, internal hydraulic replenisher, recoil buffer and two recuperator cylinders with a recoil length that varies from 700 to 1,700 mm based on the elevation of the gun. The gun tube is attached to a titanium breech block assembly using an interrupted thread which allows the gun tube to be removed and replaced from outside the vehicle.

To remove heat buildup during firing the cannon features an integral midwall cooling system which uses an electrically driven pump to circulate a 50-50 ethylene glycol-water (EGW) antifreeze mixture through a total of 24 semicircular cooling flutes cut into the outside surface of the autofrettaged steel liner which run the entire length of the barrel. The breech mechanism is a multi-lug horizontally sliding breech block with an O-ring seal and an integral pulsed neodymium: ytterbium aluminum garnet (Nd:YAG) laser ignition system for ignition of the propellant charges. After firing some of the EGW mixture is also sprayed into the chamber to extinguish residual propellant embers, clean the laser window, wet the breech seal and further cool the propellant chamber to prevent ammunition cook-off.

The cannon is designed to fire all SDI 17 cm ammunition and uses SDI's AM90 Bi-Modular Charge System (BMCS), a six-zone modular charge system consisting of low and high zone combustible-case charges containing an RDX based insensitive propellant. With a full six high zone propellant charges the muzzle velocity with a 66.8 kilogram projectile is 1,050 m/s and maximum range up to 48 kilometers with boat tailed/hollow base ammunition, 65 kilometers with base bleed ammunition, and up 85 kilometers using rocket assisted/base bleed projectiles. The cannon with modular charge system and fire-control system supports Multiple Round Simultaneous Impact (MRSI) with 8 round simultaneous impact capability at ranges up to 40 kilometers (with base-bleed ammunition) with less than 4 second time between first and last round impact. Traverse of the turret and elevation of the cannon is achieved through brushless DC servomotors with a traverse range of +/- 20° at 20°/s and elevation range of -3° to +75°at 20°/s with <0.3 milliradian pointing accuracy in both elevation and azimuth.

The cannon features an autoloader mechanism with projectile and propellant loading of the cannon being fully automated and requiring no human intervention. The cannon is fed from two projectile magazines each containing 20 fuzed projectiles stored vertically in a closed-loop conveyor located in the center of the hull and a propellant magazine containing 180 modular propellant charges which is located in the turret. When a specific projectile is selected for executing a firing mission the magazine is rotated so that the projectile moves to the center of the magazine where it can be extracted by a shuttle which grips the base of the projectile and extracts it from the magazine. The shuttle then moves the projectile to the center of the howitzer between the two magazines where the projectile is transferred onto a robotic loading arm. The shuttle includes an inductive fuze setter mechanism which automatically programs the projectile's multi-mode fuze as the projectile is transferred from the magazine to the robotic loading arm. Fuze modes includes proximity, time, point detonating and delay settings for high explosive rounds fitted with an SDI multi-mode artillery fuze or various time settings for cargo projectiles fitted with an SDI electronic-time fuze. As the projectile shuttle transfers the projectile to the robotic loading arm the propellant shuttle located in the turret extracts the desired number of modular propellant charges and loads them on to the robotic loading arm after the projectile. The robotic loading arm then rotates to align with the angle of the gun tube where a pneumatically driven flick rammer then rams the projectile and propellant charges into the cannon to be fired. The autoloader mechanism allows for a sustained firing rate of 12 rounds per minute until the onboard projectile supply is exhausted. Loading can be accomplished at any turret traverse or gun elevation angle. The ammunition supply is replenished using an accompanying resupply vehicle (RSV) which can transfer 40 rounds and 180 propellant charges to the self propelled howitzer (SPH) in less than 12 minutes while transferring fuel at a rate of 190 liters per minute to self propelled howitzer using a resupply port located at the rear of the SPH turret.

Secondary armament:For protection against close in threats the vehicle is fitted with an SDI Scanfire remotely operated weapon station mounted to the turret roof which includes an MG 45E machine gun and electro-optical sensor suite. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. The weapon station includes dual-axis gyro-stabilization to allow for effective fire while the vehicle is moving. The weapon station is traversed and elevated using brushless DC servomotors and features -15 to +70 degrees elevation and 360 degrees of traverse. The sensor system includes a CCD daylight camera with up to 10x magnification, an uncooled 640 x 480 pixel LWIR (long wave infrared) imager, and an eye-safe Nd:YAG laser rangefinder.


Protection:
Armor Protection: The chassis and turret of the vehicle are constructed from welded IRHA (Improved Rolled Homogeneous Armor) which provides all around base protection from 15 mm armor piercing ammunition. Additional ceramic composite armor protection covers the majority of the vehicle's surface including hull glacis and sideskirts and turret front, sides, and top which provides additional protection against shaped charges, explosively formed perpetrators, and high velocity shell fragments. The composite armor consists of three layers; two layers of ceramic armor and an additional layer of non-explosive reactive armor (NERA). The ceramic armor consists of hot isostatically pressed titanium diboride (TiB2) tiles embedded in a Ti-64 titanium alloy matrix. The compressive load on the ceramic tiles from the metal matrix serves to prevent the tiles from shattering, increasing multi-hit resistance. This layer of armor serves primarily to defeat kinetic energy projectiles through interface dwell; on impact the projectile erodes at the surface of the metal/ceramic matrix with no significant damage to the underlying ceramic. Two overlapping layers of titanium confined ceramic armor providing combined protection from explosively formed penetrator (EFP) submunitions and 155mm shell fragments are bolted onto the base IRHA steel hull. After the two ceramic armor layers is an outer layer of non-explosive reactive armor (NERA) which is connected to the inner RHA structure through coil springs which extend through circular cutouts in the two ceramic armor layers. The NERA layer is primarily intended to defeat shaped-charge threats and consists of two titanium-UHHS (ultra high-hardness steel) laminate plates sandwiching a layer of compressed rubber. When subject to the impact of a shaped charge jet the deformation of the rubber interlayer causes the metal plates to violently bulge and deform outwards, putting more material in the path of the shaped charge jet and causing it yaw or deflect off-course. The inside surface of the vehicle features a borated spall liner consisting of orthogonally cross-plied M5 ballistic fibers laminated into a flexible borated polyethylene resin which serves to minimize the post-armor effect of penetrating projectiles and shaped charge jets and to provide radiation protection for the crew and electronics inside the vehicle. Under-belly protection is provided by an armored V-hull which provides protection against EFP and 10kg TNT equivalent blast anti-tank mines. Additionally the three crew members located in the hull sit on blast-attenuating seats with no direct contact to the vehicle floor.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire. When a fire is detected inside the vehicle Halon 1301 contained in several pressurized bottles each with fast-reacting solenoid-actuated valves is sprayed into the compartment to extinguish the fire. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An NBC ventilation and overpressure system is also fitted to the vehicle's crew compartment as standard.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplies filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: The vehicle is equipped with SDI Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT projectiles. The system consists of a set of pre-warner radar arrays and multiple modular countermeasure modules mounted along the turret sides and roof containing electro-optical tracking sensors and directional explosive countermeasures designed to destroy or deflect oncoming projectiles before they strike the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. Six panels are arranged around the sides of the turret with another two on the turret roof which provide combined 360 degree hemispherical coverage around the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are contained in bricks on the outside of the vehicle and employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) tungsten-nickel-cobalt (WNiCo) alloy shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the turret to provide coverage over the the hull of the vehicle by steering the blast downwards or to defeat over-fly top attack projectiles by firing upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past 4 or so meters from the vehicle. The countermeasures bricks themselves employ a metal-free composite construction and are encased in a layer of thermoplastic armor to prevent the brick itself from generating any shrapnel and to protect the explosive charges from small arms fire and shrapnel and other hazards.


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The vehicle is powered by a self contained rear drive system separated from the fighting compartment by a fireproof bulkhead which includes an AMG (Arkaenisch Motorenfabrik Gesellschaft) designed HL280 diesel engine and AMG AK 7-700 hydromechanical planetary transmission, accessory drive gearbox, auxiliary power unit (APU), self-cleaning air filter (SCAF), exhaust IR suppression system, engine and APU fuel system, and the vehicle electrical system. Inlet air for the engine flows through a set of armored grills located on the sides the vehicle's engine deck before being scrubbed by a pre-cleaner and passed through a self-cleaning air filter (SCAF) where the now cleaned air then enters the engine. The exhaust from the engine is passed through an IR suppression system and then finally vented overboard through a louvered grill mounted at the rear of the vehicle. Relatively compact and designed for reliability and ease of maintenance, the vehicle's power pack has a 5,000 hour mean time between overhaul (MTBO) and air filters designed for 100 hour continuous operation at twice zero-visibility dust concentrations, can accept virtually any grade of diesel or jet fuel, can cold start at temperatures as low as -50 degrees C, and can be removed from the vehicle in as little as 15 minutes for replacement or repair.

Engine: The AMG designed HL280 diesel engine is a multi-fuel, low-heat rejection (LHR), quad-turbo diesel engine with a maximum power output of 1,765 kilowatts (2,400 PS) at its maximum rated speed of 3,300 RPM. The HL280 engine block is a monobloc design with a 60 degree cylinder bank angle and is constructed from compacted graphite iron (CGI) and features integral charge air cooler and intake manifold housings along with machined cooling passages for the synthetic oil coolant. Both the turbocharger intercooler and aftercoolers and exhaust manifolds are constructed from high-temperature stainless steel alloy and are located on the outside of the V-block with the intake manifolds integral to the V-block itself. The HL280 features a common rail electronic controlled injection (ECI) system with one piezoelectric injector per engine cylinder. Fuel is pressurized by a high-pressure, fuel lubricated hydraulic boost pump with the fuel rail mounted on the engine serving as a high-pressure accumulator. The fuel is distributed to the individual fast-switching piezoelectric injectors integrated into each engine cylinder where fuel is then injected at 2,500 bar pressure into each engine cylinder. The cylinder heads are constructed from cast ductile iron and feature black nitride coated stainless steel inlet valves and high temperature titanium/inconel alloy exhaust valves with monolithic zirconia valve seats capable of surviving the high exhaust gas temperatures of each cylinder without needing cooling. The piston in each cylinder is two piece, articulated design with a forged maraging steel crown with tungsten-carbide piston rings screwed into an aluminum skirt assembly, the steel crown of the piston cooled using a single piston oil supply nozzle located on the underside the crown. Both the cylinder head and piston crown feature a plasma-spray applied 2mm zirconia ceramic thermal barrier coating (TBC) which facilitates high temperature, high pressure engine operation with minimal thermal losses. The cylinders themselves are constructed from ductile cast iron with an aluminum-silicon carbide metal matrix composite liner with an diamond-like carbon (DLC) coating which reduces both the head temperature and the friction between the piston rings and the cylinder walls. The cylinders are cooled using synthetic oil which flows through an annular groove at the top of the cylinder in between the cylinder block and cylinder liner. The engine's crankshaft and connecting rods use an induction hardened, forged maraging steel alloy construction with diamond-like carbon (DLC) coatings to improve abrasion and corrosion resistance. The connecting rods are a telescoping design which allows for the compression ratio of the engine to be varied from 9 up to 18, allowing for the cycle isotropic efficiency to be maximized across the engine's entire operating envelope. The intake pressure of the HL280 engine is boosted via the use of four variable-geometry sequential turbochargers. The turbine of each turbocharger is a single, stage axial design constructed from silicon nitride ceramic and features a set of axially pivoting variable-area turbine vanes which open up at low engine RPMs to reduce turbo-lag and increase engine torque and then at higher engine RPMs close down to increase engine boost pressure. The exhaust turbine of each turbocharger drives both a low pressure compressor (LPC) and high pressure compressor (HPC) on a common shaft with an air-oil intercooler placed between the low pressure and high pressure stages and an air-oil aftercooler placed after the high-pressure stage of each turbocharger. Each turbocharger additionally features set of variable inlet guide vanes (VIGVs) ahead of low and high pressure compressors which prevent surge or chocking of the flow through the compressor.

Transmission: The transmission used with the HL280 engine is the AK 7-700 hydro-kinetic power shifting, reversing, and steering transmission with seven forward and three reverse gears. The transmission employs a powershift system with planetary gearing capable of shifting under full engine load, a reversing gear mechanism, and a hydrokinetic torque converter with a lock-up clutch to improve efficiency at higher speeds. Operation of the transmission is fully automatic and automatically changes gear within a range pre-selected by the driver. A digital transmission control unit (TCU) is used to control shifting in automatic mode which interfaces with the engine control unit (ECU) to control the range of the transmission. A manual override is additionally fitted which allows for range override of the transmission through a lever in the driver's compartment connected through a cable to a series of mechanical linkages attached to the shifting mechanism of the transmission. The steering drive fitted to the transmission is an infinitely variable hydrostatic/hydrodynamic superimposed differential system employing twin hydraulic drives with variable-displacement hydraulic pumps and twin hydraulic motors which are used to add or subtract power from each side of the vehicle and allow for neutral or pivot turning at infinitely variable speed. Braking functions of the transmission include a combined hydrodynamic/mechanical dual circuit integrated brake system with an internal hydrodynamic brake and external oil-cooled power assisted disc brakes on either side of the transmission. Independent service and parking brakes are additionally included. A hydraulic power take-off (PTO) system fitted to the transmission output is used to power the transmission cooling fans as well the accessory drive gearbox which contains a toroidal CVT (continuously variable transmission) which provides a constant 3,000 rpm speed output independent of engine RPM which is used to drive the vehicle's NBC compressor, alternator, self-cleaning air filter (SCAF), scavenge blower, and IR exhaust suppression system.

Auxiliary Power Unit: Auxiliary power is provided via an SDI RKM700 under-armor auxiliary power unit (APU) attached to the accessory gearbox within the engine compartment. The APU system consists of the RKM700 engine along with integral starter, fuel conditioning system, and self-contained cooling system and is used to power the vehicle's alternator, air filter compressor, and self-cleaning air filter while the engine is offline. The RKM700 APU is a single-cylinder turbocharged rotary engine with a 0.7 liter displacement which can generate a maximum of 60 kilowatts (80 PS) of power at it's rated speed of 6,000 RPM. In addition to the single-stage turbocharger the RKM700 engine features an air-to-air aftercooler and a dry-sump oil lubrication system. The RKM700 APU is oil-cooled using an integral oil-air heat exchanger and cooling fan. The APU is fed from the main engine air inlet and exhausts though a grille in the upper left hull sponson.

Electrical System: The vehicle's electrical system interfaces with the engine and transmission, CVT accessory drive gearbox, self-cleaning air filter (SCAF,) APU, NBC filtration system, HVAC system, fuel system, and fire suppression system. The electrical system is consists of four 170 amp-hour lithium-ion batteries, battery heater system, electrical distribution system, and a 1,000 amp, 28 kilowatt oil-cooled brushless permanent magnet alternator driven by the APU or main engine through the CVT accessory drive gearbox. The lithium-ion batteries are wired in series-parallel and provide 680 amp-hours capacity of 24 VDC output from -40 degrees to +50 degrees C ambient temperature and allow for engine cold start at -40 C without the APU after up to four hours of silent watch. The batteries are charged using the 1,000 amp oil-cooled alternator through a solid-state voltage regulator which at an alternator speed of 3,000 rpm delivers 28-30 volts of DC power at up to 150 amps to rapidly charge the batteries.

Suspension & Running Gear: the vehicle uses an SDI designed semi-active in-arm hydro-pneumatic suspension system with four sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (16 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The vehicle uses a decoupled running gear design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle employs double-pin, twin center guide tracks with removable rubber road-pads. Track width is 75 centimeters with a pitch of 20 centimeters with a total of 88 links per track. To reduce weight the vehicle's track links and pins employ a novel composite construction using a particle reinforced titanium metal matrix composite in place of traditional steel. The track parts are formed through powder metallurgy using titanium carbide (TiC) particles mixed into Ti-6Al-6V-2Sn (Ti-6-6-2) alloy powder, the final composite parts offering superior corrosion and wear resistance to steel parts while reducing track weight approximately 25% over an equivalent strength steel design. Each track link is fitted standard with twin detachable road pads constructed from a kevlar-natural rubber composite to reduce noise and road wear. For traversing icy ground up to 44 steel cleats can be fitted to each track, one cleat replacing the rubber pad on every fifth track link, the cleats being stored on the vehicle's glacis when not in use. The vehicle's sixteen road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units.


Sensors & Fire Control:
Projectile Tracking System: The Projectile Tracking System or PTS is a phased array radar system which measures the muzzle velocity of each round as it departs the cannon and then tracks it in flight in order to compute it's impact point, allowing the fire control system to make corrections for subsequent shots. The PTS consist of an inerferometer array mounted on the front face of the turret which includes one 512 element transmit array with a maximum transmission power of 500 watts and four 512 element receive arrays operating in the Ku band (15-17 GHz) using gallium-nitride (GaN) transmit and receive modules.The PTS is capable of tracking up to six projectiles in flight simultaneously from the muzzle to a range of up to 100 kilometers and can determine projectile muzzle velocity to within 0.05% error with a range accuracy of less than 0.2 meters, doppler velocity accuracy of less than 0.02 meters per second, and has a projectile impact prediction accuracy capability of less than 15 meters at a range of 50 kilometers. The PTS is also capable of communicating with rounds in flight with the option of varying fuze settings before projectile impact or submunition release through the use of a one-way RF datalink included in SDI course-correcting artillery fuzes.

Gun Laying and Positioning System: the vehicle employs a fully digitized gun positioning and laying system (GLPS) mounted on the gun cradle which uses a combination of GPS and inertial navigation sensors (INS) to automatically compute gun direction, position and elevation above sea level. The GLPS along with input from the vehicle's onboard vehicle motion sensors (VMS) additionally acts as the vehicle's navigation system. The GPLS includes an inertial sensor suite with shock hardened 3-axis fiber-optic gyrocompass and 3-axis accelerometer, 3-axis magnetometer, odometer, and 24 channel differential Selective Availability Anti-spoofing Module (SAASM) based GPS system which provides sub-meter horizontal and vertical position accuracy. The GPLS can operate in hybrid INS+GPS mode, GPS only, or INS only (with slightly reduced accuracy) modes and provides linear and angular acceleration, linear and angular velocity, position and attitude information to the vehicle's fire control and navigation system as well as true, grid or magnetic heading calculation and position updates which are displayed to the crew on their multi-function displays in real time. A RF datalink link allows the gun laying system to be data-linked to a the artillery batter command post which enables target position and ammunition data to be received and fire missions automatically carried out from unprepared positions.

Electro-Optical Direct Fire Sight : Mounted above and to the left of the gun cradle is a 2-axis stabilized electro-optical targeting system which provides for the observation, tracking, and targeting of line-of-sight targets. The system consists of a 3rd generation long wave (LWIR) thermal camera with 1280 x 1024 px resolution and 1.75° to 26°horizontal field of view, color CMOS daylight camera with 1920 x 1080 px resolution and 1.5° to 30°horizontal field of view, eye-safe 2.08 μm Holmium laser rangefinder (LRF), and 1.06 μm Nd:YAG laser designator. A ballistic computer integral to the sight provides for lead-angle computation against moving targets along threat geo-localization using the vehicles onboard INS/GPS system. The electro-optical gun sensor system is enclosed by a ballistic cover to protect it from shrapnel and small-arms fire and can be elevated from -15° to +65°.


Situational Awareness:
Driver Vision Enhancer: the vehicle includes both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 14 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55 x 40 degree field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted to the turret roof each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions. Each STAS module also contains an imaging sensor autoprocessor (ISA) similar to the one in the gunner and commander FLIR sights which provides automatic target recognition (ATR) capability of threats detected by the system. The STAS can be used to monitor the area around the vehicle during silent watch or while the crew is asleep and includes automatic alert broadcast and target-tracking/moving-target indicator functions which can track detected threats and can interface with the fire control system to hand-off threats to the remote-control weapon station or to the direct-fire optic for close-range engagement by the vehicles primary or secondary weapons. armament.


Communications:
Vehicle Multiband Networking Radio:The vehicle is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.


Battle Management:
SDI Wotan Fire Support System: The Chimera self-propelled howitzer is fitted as standard with SDI's Wotan Fire Support System (FSS), an integrated artillery and fire support command and control system based on SDI's Arcturus Battle Management System (ABMS) which combines real time computing and battlefield networking capability to coordinate multiple fire missions on different weapons platforms simultaneously. The Wotan FSS hardware installation in the vehicle consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's VHF/UHF multiband networking radio which is used to establish the vehicle as a node in the Arcturus/Wotan network. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbiology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus/Wotan equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus/Wotan network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units.

The Arcturus/Wotan network employs a self-forming / self-healing time-division multiple access (TDMA) mobile ad hoc network (MANET) formed using SDI's family of software defined VHF/UHF multiband networking radios which connects every howitzer, mortar, rocket and missile launcher, strike aircraft, warship, artillery command post, and forward observer in a theater of operations as a series of nodes in the MANET. The Wotan system then provides fire support planning, fire support mission execution, movement control, field artillery mission support and field artillery fire direction operations using decentralized edge computing with the computing capability of each node in the network uses to provide the processing requires to simultaneously execute each computing task of the system across an entire theater of operations. When a fire mission request is received the network processes the request using a decision-tree programmed as a set of cascaded if-then-else statements which establishes pre-set rules for achieving the desired target effects (obscure/suppress/neutralize/destroy) against a set of pre-defined target types and characteristics. The network will first compute the type and number of rounds or missiles to achieve the desired effects on each target as a function of the target types, hardness, distance from each available fire support aspect, and local meteorological conditions. The network will then determine the priority of each fire support mission as a function of target type and location and then assign the fire missions in descending priority to fire support assets in the theater as a function them having the type and quantity of munitions to fulfill the specific fire request and their proximity to each target. The use of edge computing allows the system to function without a dedicated battery HQ node with each battery of like fire support assets slaved together into a tactical local area network (LAN) in the overall Arcturus/Wotan network and used to aid in the processing of its own fire missions using the Wotan/Arcturus processor module installed in each fire support vehicle. Each fire support asset in each LAN is able to then assign itself a preference for potential fire missions as a function of the asset's firing capability, munitions available, and location in order to allow the Wotan/Arcturus to more efficiently assign missions to the fire support assets in the Wotan/Arcturus network.


AI Modules:
To aid in the performance of the crew the vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, and C3 (command, control, and communications)

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. For example if the system receives an track report than an enemy vehicle(s) are moving along a road it will assume that the vehicle(s) have not detected the presence of own or friendly forces and will keep moving down the road. On the other hand if another track report is received indicating that the enemy vehicle(s) have moved off-road and actively engaging with their armament the system will assume that own or friendly forces have been detected and that the targets will attempt to retreat and form a defilade position. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.
Last edited by The Technocratic Syndicalists on Fri Nov 04, 2022 5:01 pm, edited 72 times in total.
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Postby The Technocratic Syndicalists » Sun Nov 11, 2018 8:25 pm

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PzM 303 Griffon

General Characteristics:
  • Type: Self propelled mortar
  • Weight: 34.0 t
  • Length (hull): 6.8 m
  • Width: 3.4 m
  • Height: 2.7 m
  • Crew: 4 (driver, gunner/commander, two loaders)

Mobility:
  • Engine: 2x AMG HL44 multi-fuel diesel engines, 400 kW (550 PS) each
  • Transmission: Diesel-electric; 2x 300 kW traction motors, 2x 150 kW steering motors
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 950 l
  • Operational range: 750 km

Armament:
  • 1x 12 cm SDI GWS120 L/25 twin-barrel breach loading mortar, 80 rounds
  • 1x 8 mm MG-45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 29.4 PS/t (21.8 kW/t)
  • Ground clearance: 0.50 m
  • Ground pressure: 0.70 kg/cm2
  • Gradient: 60%
  • Sideslope: 30%
  • Fording depth: 1.5 m
  • Trench crossing: 2.6 m
  • Vertical wall climb: 1.1 m


Overview
The Panzermörser 303 (PzM 303) Griffon is an armored, tracked self-propelled mortar designed by SDI Vehicle Systems. The Griffon employs a chassis derived from SDI Vehicle System's PzKfz 303 armored personnel carrier and consists of a modified PzKfz 303 chassis fitted with a turret containing a twin-barrel breach-loading 12 cm mortar and ammunition autoloading system.


Armament
GWS120 Automatic Mortar:
[*]Caliber: 120 mm
[*]Weight: 4,400 kg (turret)
[*]Traverse: 360°
[*]Elevation: -3° to +85°
[*]Ammunition: 48 rounds (bustle) + 32 rounds (hull)
[*]Rate of fire: 24 rounds/min
[*]Range: 10 km (standard), 16 km (rocket assisted)[/list]
The primary armament of the vehicle is an SDI Armament System's GWS120 automatic mortar system, a double barreled, breach loading, smoothbore mortar system housed in an unmanned turret located at the rear of the vehicle. The weapon fires standard smoothbore 12 cm mortar projectiles modified with a short stub case which acts to seal the breach during firing. Each barrel is 25 calibers (3 meters) long and features an electro-deposited hard chrome plating along its entire length to reduce wear. Each barrel is contained in an independently recoiling hydro-pneumatic sleeve which allows both barrels to be fired independently. Each tube employs a semi-automatic breech mechanism with a vertically sliding wedge breech mechanism. Positive obturation is provided by small stub case attached to the base of each projectile which is automatically ejected after firing. Each breech mechanism includes an integral pulsed neodymium: ytterbium aluminum garnet (Nd:YAG) laser which is used to ignite the propellent attached to each projectile. After firing a 50-50 EGW (ethylene-glycol water) antifreeze mixture is sprayed into the chamber to extinguish residual propellant embers, clean the laser window, wet the breech seal, and to prevent ammunition cook-off by cooling the walls of the chamber.

The GWS120 mortar system includes a autoloader system with three fully automated carousel style projectile magazines. Two magazines each containing 24 fuzed projectiles with attached propellant charges are towed horizontally in closed-loop conveyors are are located inside the turret bustle with an additional magazine containing 32 fuzed projectiles with attached propellant charges stowed vertically in the hull underneath the turret. When a specific projectile is selected for a firing mission one of the bustle magazines is rotated so that the correct projectile moves to the center of the magazine where it can be exacted by a shuttle which grips the base of the projectile and extracts it from the magazine. The shuttle then moves the projectile to the center of the bustle between the two magazines where the projectile is transferred onto one of two robotic loading arms (one for each barrel). The shuttle includes an inductive fuze setter mechanism which automatically programs the projectile fuze as the projectile is transferred from the magazine to the robotic loading arm. While the projectile is on the robotic loading arm the human loader is responsible for setting the correct propellant charge increment. The robotic loading arm then rotates to align with the elevation of the gun tube where a pneumatically driven flick rammer then rams the projectile into the breech to be fired. Once the bustle ammunition supply is exhausted the weapon will feed from hull magazine which includes an additional projectile shuttle which extracts projectiles from the hull magazine and then rotates them to along with the angle of the turret before the projectile is transferred onto one of the robotic loading arms. The autoloader mechanism allows for a firing rate of up to 24 rounds per minute at any turret elevation or traverse angle with minimal physical intervention by the crew.

Scanfire RWS: The turret of the vehicle is fitted with an SDI Scanfire remotely operated weapon station . The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers.

Smoke-grenade launchers: The vehicle is equipped with a total 8 smoke grenade launchers grouped into two 4-tube launchers on either side of the vehicle's turret which cover the forward two 90º sectors. The smoke launchers fire 66mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The launchers are controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each forward 90 degree sector.


Protection:
Armor Protection: The hull of the vehicle is constructed from friction stir welded (FSW) 2139-T8 aluminum alloy plates 40 mm thick which provides the hull 360° protection against 14.5 mm AP ammunition at 200 meters and 155 mm high explosive shell fragments at 30 meters. The base armor is augmented by ceramic armor panels containing tandem silicon-carbide (SiC) tiles embedded into a cast 7075 alloy aluminum matrix which along with the base armor provide frontal arc protection (+/- 30°) against 30 mm APFSDS rounds at 500 meters and 360° protection against 152 and 155 mm high explosive shell fragments at 10 meters. The turret is constructed from welded ultra high hardness steel (UHHS) armor and is fitted with ceramic armor panels which give the turret the same protection level as the hull. The inside surface of the vehicle features a borated spall liner consisting of orthogonally cross-plied M5 ballistic fibers laminated into a flexible borated polyethylene resin which serves to minimize the post-armor effect of penetrating projectiles and shaped charge jets and to provide radiation protection for the crew and electronics inside the vehicle. Under-belly protection is provided by an armored V-hull which provides protection against EFPs and 10kg TNT equivalent blast anti-tank mines. Additionally the four vehicle crew members located in the hull sit on blast-attenuating seats with no direct contact to the vehicle floor.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFSS) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire. When a fire is detected inside the vehicle Halon 1301 contained in several pressurized bottles each with fast-reacting solenoid-actuated valves is sprayed into the compartment to extinguish the fire. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Propulsion
  • Name: HL44
  • Type: Multi-fuel diesel engine
  • Length: 890 mm
  • Width: 450 mm
  • Height: 740 mm
  • Dry Weight: 450 kg
  • Bore/stroke: 115/105 mm
  • Displacement, cylinder: 1.1 l
  • Displacement, total: 4.4l
  • Charging method: two-stage variable-geometry turbocharger
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 4, inline
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 400 kW @ 4,300 RPM
  • Torque: 920 N-m @ 3,800 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Griffon employs a diesel-electric drive system consisting of twin diesel engines and integrated starer/generator units places in the hull sponsons and a mechanically regenerated hybrid electro-mechanical cross-drive transmission located in the front of the hull which combines the power input of the traction and steering motors and distributes it to the twin drive sprockets. The mechanical decoupling of the diesel engines with the drive sprockets allows for the engines to run at a constant RPM, improving fuel efficiency, while the use of two diesel propulsion units and twin steering and traction motors in the transmission provides a high level of redundancy and resistance to damage. The packaging of the diesel engines in the hull sponsons also serve to increase the effective internal volume of the hull for crew, weapons, and other payload.

Engine: The engine used in each powerpack is an AMG (Arkaenisch Motorenfabrik Gesellschaft) HL44, a four cylinder inline, common rail fuel fuel injection, twin sequentially charged low-heat rejection diesel engine which outputs a maximum 400 kW of power at 4,300 rpm. The engine also includes an integral oil-cooled permanent magnet synchronous flywheel starter-generator unit which is geared to the engine output shaft using a speed-increasing transfer case with a fixed 4.2:1 gear ratio. The HL44 employs a common rail fuel-injection system with a fuel rail running the length of the engine and twin hydraulic boost pumps running at up to 3,100 rpm to pressurize the fuel to 1,800 bar for injection into each cylinder. Turbocharging is accomplished with twin single-stage variable-geometry turbocharger units using variable-area turbine nozzles which providing boost pressure ratios up to 5:1. A water-to-air charge-air cooler is placed after the turbocharger compressor stages to cool and density the air before entering the combustion chambers. To maximize engine performance across a broad ambient temperature spectrum the water and oil cooling system of the engine are split into a high temperature loop which cools the piston liners, cylinder heads, and other engine components along with the first stage of the charge-air cooler, and a low temperature loop which cools the power electronics, engine oil, and the second stage of the charge-air cooler. A dual-circuit water pump circulates cooling water through both the high and low temperature loops and then through the radiator cooling system which employs twin 30 kilowatt variable-speed fans to cool the coolant before it's passed into the expansion tank and then circulated again through the twin coolant loops. An integrated flywheel starter generator is used to start the engine and is rated for mechanical input power of up to 400 kW and outputs 3 phase 60 Hz 600 VAC alternating current The starter-generator is a self-excited, brushless, oil cooled, permanent magnet machine using neodymium-iron-boron permanent magnets and has a rated speed of 18,000 RPM, necessitating a 4.2:1 gear ratio speed-increaser gearbox be placed between the generator and engine. Other engine accessories including inlet air filter system, turbo intercooler and aftercooler circuits, charge air cooler with inlet manifold, exhaust scrubber and infrared suppression system, and oil filter and cooler, are included in the power pack as a single engine unit. The left and right hand side powerpacks are identical and can be fitted to either side of the vehicle. The powerpack additionally includes the oil cooling system with air-oil heat exchanger and a hydrostatically driven cooling fan.

Transmission: The vehicle powertrain system employs a mechanically regenerated cross-drive transmission which reduces the required motor power required to drive and regeneratively brake each drive sprocket. The transmission system includes twin 150 kilowatt oil-cooled permanent magnet synchronous steering motors and twin 300 kilowatt oil-cooled permanent magnet synchronous traction motors located on either sides of the transmission. Both traction and steering motors employ a rotor with samarium-cobalt magnets and a ferromagnetic core with an inconel superalloy sleeve and have a maximum rated speed of 18,500 RPM with a 93% efficiency at a base speed of 4,600 RPM. The steering and traction motors on either side of the transmission are supplied electrical power through a generator converter box located in each sponson ahead of the the powerpack which converts the three phase 600 volt AC power from the engine generators into 600 volt DC power which is transferred to a DC bus located on either side of the cross drive unit which then supplies DC power to the motor inverters and the various accessory drives. The cross drive unit itself contains a central drive shaft connected to a differential gearbox which combines the inputs from the two steering motors and two traction motors to power the drive sprockets through the planetary reduction final drive assemblies located on either side of the cross-drive transmission. A two speed oil-cooled planetary reduction gearbox with twin hydraulically actuated clutches is additionally incorporated into the cross-drive transmission and connects the central differential to the steering and traction motors to reduce the required rpm and torque ranges of the electrical steering and traction motors. The cross drive additionally contains an oil cooled wet disk brake and a parking brake unit.

Suspension & Running Gear: The suspension system used by the vehicle is an SDI designed semi-active in-arm hydro-pneumatic suspension system with three sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (12 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The vehicle's running gear features a decoupled design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle's road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units. Instead of conventional steel tracks the vehicle employs composite rubber band tracks which are 50% lighter and result in a 70% vibration reduction and 10 dB noise reduction inside the vehicle at a road speed of 50 kph. The tracks are 550 mm wide with a 120 mm pitch and have a designed durability of over 5,000 km before needing replacing.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 6:43 pm, edited 42 times in total.
SDI AG
Arcaenian Military Factbook
Task Force Atlas
International Freedom Coalition


OOC: Call me Techno for Short
IC: The Kingdom of Arcaenia

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The Technocratic Syndicalists
Minister
 
Posts: 2173
Founded: May 27, 2015
Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Sun Nov 11, 2018 8:49 pm

Image

RS 90 Firestorm

General Characteristics:
  • Type: Multiple rocket launcher
  • Weight: 45,000 kg
  • Length: 11.7 m
  • Width: 2.5 m
  • Height: 3.2 m
  • Crew: 2

Mobility:
  • Engine: AMG HL80 turbocharged V8 diesel, 735 kW (1,000 PS)
  • Transmission: Diesel-electric transmission; 735 kW AC generator, 10x 100 kW hub motors
  • Suspension: Hydropneumatic
  • Brakes: Disc brakes with ABS (Anti-Lock Braking System)
  • Tires: 10 (+1) 16R20 with run-flats and CTIS (Central Tire Inflation system)
  • Steering: 5-axle with power assist
  • Max road speed: 115 km/h
  • Fuel capacity: 950 l
  • Operational range: 1,000 km
  • Ground clearance: 0.60 m

Armament:
  • Caliber 280 mm
  • Number of tubes: 12
  • Firing range: 20-200 km

Maneuverability:
  • Gradient: 70%
  • Side slope: 40%
  • Fording Depth: 1.5 m
  • Trench Crossing: 2.5 m
  • Vertical Wall Climb: 0.6 m


Overview
The Raketensystem 90 (RS 90) Firestorm is a self propelled rocket artillery vehicle deisgned by SDI Vehicle Systems. The RS 90 employs a trainable loader-launcher module (LLM) capable of firing SDI's family of 280 mm artillery rockets or SDI's Archer tactical ballistic missiles.


Armament
The vehicle's primary armament consists of a self-loading rocket launcher which can carry either 12 280 mm RS 90 artillery rockets or four RBS 81 Archer tactical ballistic missiles. Rockets are carried in 6-cell rocket launch pods and Archer missiles carried in 2-cell missile launch pods with identical external dimensions to the rocket pod of which two can be loaded into the vehicle's launcher-loader module (LLM). All 12 rockets or four missiles can be fired in less than 60 seconds and can be reloaded in less than 3 minutes using two electric boom and hoist assemblies mounted above the launch pod containers. The launcher-loader module uses an electro-hydraulic launcher drive system driven by engine power take-off (PTO) with two 350 bar hydraulic motors which can traverse the launcher-loader module 190° left or right of center at a rate of 10° /sec and can elevate it from 0° to +60° at a rate of 20°/sec. In addition to the rocket and missile pods the launcher-loader module also contains a 24V power supply for the rocket/missile electrical firing system and an integral fire control system including an electronics unit (EU), fire control unit (FCU), a boom controller (BC), short/no-voltage tester (SNVT), stabilization reference package/position determining system (SRP/PDS), meteorological data system (MDS), meteorological measuring set (MMS), payload interface module (PIM), program load unit (PLU), and communications processor (CMP).


Protection:
Armor protection: The HTTS chassis used by the RS 90 vehicle features a fully armored cab constructed from welded 5 mm 600 BHN hardness ultra-high-hardness steel (UHHS) plates with integral silicon carbide (SiC) ceramic/polyethylene (UHMWPE) composite armor panels, ballistic glass windows, and an inner M5 fiber/epoxy composite spall liner which provides 360º azimuth and 0 - 30°elevation protection against 7.62 mm tungsten core armor piercing ammunition at a distance of 30 meters and 155 mm high explosive shell fragments at 60 meters. Under body protection for the crew cab consists of a multi-layered internal V-hull with a kevlar floor lining and mine blast protective crew seats which is designed to withstand a 10 kg TNT equivalent explosive blast AT Mine denoting under center or an 8 kg TNT equivalent explosive mass AT Mine detonating under one of the wheels.

Fire extinguishing system: The crew cab, fuel tanks, and powertrain compartments of the HTTS include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew cab are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the floor of the crew cab which through a series of hoses and pipes spray Halon agent into the crew or engine compartment when the system detects a fire. The system can also be manually activated through a panel near the driver's seat. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew cab and maintains cab pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing absorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Mobility
  • Name: HL80
  • Type: Multi-fuel diesel engine
  • Length: 1,080 mm
  • Width: 700 mm
  • Height: 760 mm
  • Dry Weight: 830 kg
  • Bore/stroke: 109/107 mm
  • Displacement, cylinder: 1.00 l
  • Displacement, total: 8.00 l
  • Charging method: Twin variable-geometry turbochargers
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 8, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 210 g/kW-hr
  • Power: 735 kW (1,000 PS) @ 4,250 RPM
  • Torque: 2,050 N-m @ 2,750 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Sensors & Electronics:
Panoramic Driver Vision Enhancer: For driving at night or in low-light level conditions the cab of the HTTS chassis of the vehicle is fitted with a SDI Panoramic Driver Vision Enhancer (PDVE) module which contains three 640 x 512 pixel 17 µm uncooled vanadium oxide (Vox) microbolometer sensors operating in the LWIR band (8-12µm) which combined provide a stitched 140° horizontal by 30° vertical field of view ahead of the vehicle. HDMI output from the panoramic DVE sensor is streamed at 30 Hz to an 800 x 600 pixel resolution driver’s vision enhancer (DVE) display & control module located on the vehicle dashboard which allows the driver to pan the entire 140° field of view with the DVE output scaled to the full display size.

Vehicle Multiband Networking Radio: For C4I and communications purposes the vehicle is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable unter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.

Integrated Driver Assist System: The HTTS chassis used by the RS 90 launcher vehicle comes standard fitted with SDI's Integrated Driver Assist System (IDAS) system which includes forward collision warning (FCW), emergency brake assist (EBA), adaptive cruise control (ACC), lane departure warning (LDW), electronic stability control (ESC), and blind spot monitoring functions.

Forward collision warning (FCW) and emergency brake assist (EBA): The forward collision warning (FCW) and emergency brake assist (EBA) system employs a front facing 77 GHz millimeter wave (MMW) radar in the front bumper which is intended to detect moving and stationary vehicles or pedestrians in the vehicle's path. The system will then generate both audible and visual warnings and if necessary will automatically brake and de-throttle the engine if the driver does not react in time. Should the driver apply the brakes with insufficient force a dynamic brake support (DBS) system will increase the brake force above what the driver has applied in order to avoid a collision.

Adaptive cruise control (ACC): The adaptive cruise control (ACC) system employs the forward facing 77 GHz MMW radar along with a 24 GHz ground speed radar mounted with a 35° look down behind the forward wheel well and automatically adjusts the vehicle speed to maintain a safe distance from vehicles ahead on the road. The adaptive cruise control system is controlled by a lever attached to the steering column. Gently tapping the lever either up or down engages the adaptive cruise control and increases the cruise speed by one kilometer per hour. Pushing or depressing the lever further increases or decreases speed by five kilometers per hour. A knob on the lever is used to adjust following distance in one meter increments which is displayed on the central screen in front of the driver. Pushing the lever forward, braking, or accelerating will disable the adaptive cruise control.

Lane departure warning (LDW): The lane departure warning (LDW) system employs two sets of CCD cameras on either side of the crew cab which track the lane markings on either side of the vehicle and provide both an audible and visual warning to the driver when one of the lane markings is crossed without the turn signal being applied.

Electronic stability control (ESC): The electronic stability control (ESC) system is designed to mitigate severe oversteer or understeer conditions leading to vehicle loss of-control (LOC) as well as mitigating on-road rollovers by using a lateral acceleration sensor, yaw rate sensor, and steering wheel angle sensor to monitor the vehicle’s directional control and selectively applying the brakes at each wheel position and reducing engine power in order to help the driver regain control of the vehicle. The ESC will also maintain heading control by determining the driver’s intended heading via the speed and steering wheel angle sensors and automatically adjusting the steering behavior of the vehicle if the steering response does not match the driver’s intention.

Blind spot monitoring: The blind spot monitoring system employs two side looking 24 GHz short-range radars mounted either side of the crew cab with a 160° field of view which will generate a visual warnings for the driver when the radars detect the presence of cars or pedestrians located in one of the vehicle's blind spots. The system will generate an additional audible warning if the driver activates the turn signal while the system has detected an object in one of the vehicle's blind sports and will increase the resistance in the steering wheel if a driver attempts to change lanes while the system has detected an obstacle in one of the blind spots.
Last edited by The Technocratic Syndicalists on Wed Jul 20, 2022 8:32 am, edited 33 times in total.
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The Technocratic Syndicalists
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Postby The Technocratic Syndicalists » Mon Nov 19, 2018 11:02 pm

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MiRpz 341 Ogre

General Characteristics:
  • Type: Assault breacher vehicle
  • Weight: 77.1 t
  • Length: 7.9 m
  • Width: 3.8 m
  • Height: 2.6 m
  • Crew: 3 (driver, gunner, commander) or 1 remote operator

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,300 l (340 Gallon)
  • Operational range: 550 km

Armament:
  • Caliber 345 mm
  • Number of tubes: 24
  • Rocket weight: 105 kg
  • Warhead weight: 60 kg
  • Firing range: 1,000 meters

Maneuverability:
  • Power/weight Ratio: 33.5 PS/t (24.6 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.95 kg/cm2
  • Gradient: 70%
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
The Minenräumpanzer 341 (MiRpz 341) Ogre is an optionally manned minefield and obstacle breaching vehicle designed by SDI Vehicle Systems. The vehicle consists of aPzKpfw 151 Tiger chassis fitted with a lane marking system and either a mine plough, dozer blade, or other engineering attachments and a armored superstructure with limited traverse which contains a 24 tube rocket launcher used for mine clearing and breaching purposes.


Armament:
34 cm WS 130
  • Type: Unguided Rocket
  • Length: 2,550 mm
  • Diameter: 345 mm
  • Weight: 105 kg
  • Speed: 230 m/s
  • Range: 4.5 km
  • Propulsion: solid-fuel rocket
  • Warhead weight: 60 kg
The primary armament of the vehicle is a 24-tube rocket launcher mounted to the back of the superstructure which is designed to fire 34 cm WS 130 rockets. The superstructure is similar in shape to the turret of the PzKpfw 151 and features limited 60 degree traverse with +/- 30° traverse along either side of the vehicle centerline. Each WS 130 rocket consists of a 34.5 cm diameter cylindrical fuel-air explosive warhead with a nose mounted fuze containing 45 kilograms of ethylene oxide which is attached to a 21.5 cm diameter rocket motor and stabilized in flight by a circular tailfin and by angled vanes in the rocket motor nozzle which impart spin onto the rocket at launch. The warhead initiated by an impact fuze at the end of a 185 meter centimeter probe which extends at launch from the front of the warhead which detonates a small bursting charge running along the center of the warhead which disperses the ethylene oxide fuel as an aerosol cloud which mixes with the surrounding air. A second, larger explosive charge is then detonated 0.15 seconds later, igniting the aerosol cloud and creating a large explosion with a very high overpressure on the target. The blast overpressure from the warhead is sufficient to destroy surface-laid mines within a radius of 10 meters and mines buried under 15 centimeters of soil within a radius of 6 meters. The rockets can be fired individually or can be ripple fired in intervals from 1.0 seconds to 9.9 seconds in 0.1 second intervals. When firing all 24 rockets in sequence to create an overlapping linear array of detonations the system is capable of clearing a path around 200 meters long and 8 meters wide through a minefield at ranges up to 700 meters from the vehicle. Alternatively the vehicle can be used a short-range rocket artillery system with each rocket having a maximum ballistic range of 1,000 meters.

Secondary armament: For protection against close in threats the vehicle is fitted with an SDI Scanfire remotely operated weapon station mounted to the superstructure roof which includes an MG 45E machine gun and electro-optical sensor suite. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. The weapon station includes dual-axis gyro-stabilization to allow for effective fire while the vehicle is moving. The weapon station is traversed and elevated using brushless DC servomotors and features -15 to +70 degrees elevation and 360 degrees of traverse. The sensor system includes a CCD daylight camera with up to 10x magnification, an uncooled 640 x 480 pixel LWIR (long wave infrared) imager, and an eye-safe Nd:YAG laser rangefinder.

Smoke-grenade launchers:For obscuration purposes the vehicle is equipped with a total 32 smoke grenade launchers grouped into four groups of four on each side of the superstructure covering the front two 90 degree sectors. The smoke launchers fire 66mm diamater red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. .The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each frontal 90 degree sector.


Breaching Equipment:
Hydraulic Equipment Adaptor: For attaching front-end engineering equipment such as mine plows or bulldozer blades the hull of the Ogre is fitted with an SDI Hydraulic Equipment Adaptor (HEA). The HEA is mounted to the glacis of the vehicle and contains an on-board electro-hydraulic system with an integrated hydraulic pump, motor and control system which allows hydraulically actuated engineering equipment to be rapidly attached and detached from the vehicle without tools. The HEA also has a hydraulic rapid jettison system which allows any accessory attached to the HEA to be jettisoned in the case of battle damage to the attached accessory. The HEA is attached to the upper and lower glacis plates via a set of locking pins and can be fitted onto or removed from the vehicle in about 15 minutes. The functions of the HEA are controlled from a display unit and joystick located inside the driver and commander's compartments which is used to control the various engineering attachments which can be attached to the HEA.

Articulated Mine Plow: For clearing buried minefields the vehicle is fitted with an SDI Articulated Mine Plow (AMP), a blast resistant V-shaped full-width mine plow which lifts concealed or buried mines to the surface and pushes them clear to the side of the vehicle as it advances forward. The AMP attaches to the Hydraulic Equipment Adaptor (HEA) and is designed to be used at vehicle speeds of 6 to 15 km/h and when in use limits the vehicle to a grade of 45% and a sideslope of 40%. The AMP has three hydraulically blade actuated sections; a center V-shaped blade with seven tines and two left and right side track width blades also with seven tines each. The outer blade sections are extended hydraulically before operation with the AMP having a width of 3.8 meters in the stowed position and 4.5 meters in the extended position. The depth of the mine plow is maintained by an automatic depth control system which uses three aluminum alloy plow skids supported by hydraulically actuated skid arms, one for each mine blade section, which remain in constant contact with the ground ahead of the mine plow. The skids ensure the individual mine plow sections accurately follow the terrain contour using a automatic depth control system which employs an ultrasonic sensor in each skid connected to a closed-loop control system which actuates the mine plow sections to ensure a constant mine plow depth. The mine plow depth is set either by the driver or commander using a control display in the driver's compartment or via remote control (when operated remotely) and is varied as a function of terrain and the specific mine threat environment with a default depth of 35 centimeters. For countering magnetic mines the articulated mine plow is fitted with a Magnetic Signature Duplicator (MSD) system which safely detonates magnetic influence mines ahead of the vehicle. The MSD is run off the vehicle's 28 VDC power system and consists of four emitter coils, two power boxes and a MSD Control Unit (MSDCU) which is located inside the driver's compartment of the vehicle.

Dozer Blade: For earthmoving and obstacle clearing operations the vehicle can be fitted with a dozer blade which like the Articulated Mine Plow (AMP) attaches to front of the vehicle using the Hydraulic Equipment Adaptor (HEA). When equipped with the dozer blade the Ogre can be used for various engineering tasks including creating hull-down positions for gun tanks, digging gun emplacements, breaching defensive earthworks, creating and filling anti-tank ditches, clearing road blocks and rubble, and clearing unexploded ordnance.The dozer blade is 4.5 meters wide with the hydraulically deployed wing extensions (3.5 meters wide in the stowed position) and is designed to move earth, rubble and obstacles with the ability to dig up to one meter into the ground at a swipe and excavate 400 m³ of earth per hour. The dozer blade is also heavily armored and is designed to withstand mine damage. The blade controlled by either the driver or commander or remotely using a joystick which controls the roll, pitch, and height of the dozer blade with three pre-set operation positions including stowed, deployed, and float.

Lane Marking System: To mark cleared lanes through minefields the vehicle is fitted with a Lane Marking System (LMS) mounted to the rear of the the chassis behind the engine deck which fires luminescent marker poles into the ground behind the vehicle at controlled intervals. The LMS consists of left and right dispenser units, an air compressor unit, and a LMS control unit mounted at the driver position inside the vehicle. Each dispenser unit contains 50 1.0 meter long fluorescent darts which are fired into the ground using pneumatic pressure supplied by a variable speed air compressor. The variable speed air compressor provides various launch pressure settings which enable the darts to penetrate various types of surfaces and terrain including sand, soil and gravel, asphalt, or concrete. The darts can fired either manually or automatically in either time or distance based intervals using the control panel in the driver's compartment.


Protection:
Armor Protection:The MiKpfw 341 Ogre employs the same heavy-metal composite armor system as fitted to the PzKpfw 151 main battle tank which is designed to provide protection against kinetic energy (KE) threats in the form of long-rod penetrators fired by high-pressure tank cannons and chemical energy (CE) threats including large-caliber shaped charge munitions. The composite armor covers the front and sides of the superstructure and the front and the sides of the hull with the remainder of the vehicle protected only by conventional steel armor. The line-of-sight (LOS) thickness of the armor of the vehicle measures 1,300 mm meters across the glacis and superstructure front and 700 mm across the frontal superstructure sides. The armor is designed to provide frontal /- 30° protection against large caliber tank gun fired APFSDS rounds (800-1000 mm RHA penetration) and large caliber anti-tank guided missiles (~170mm diameter SC with 1500-1600 mm RHA penetration) and 360° protection against 15mm AP ammunition and handheld anti-tank weapons (110mm diameter SC). Appropriate average RHA equivalent protection for the glacis and superstructure armor across the frontal 60 degree arc is 1,000-1,200 mm RHA against kinetic-energy munitions and 1,800-2,200 mm versus chemical-energy munitions. The armor in the glacis is structurally integrated into the hull and side skirts of the vehicle while the superstructure composite armor is contained in a series of armor modules which bolt onto the front and sides of the superstructure. The armor modules are designed to be replaced in field when damaged and can additionally be opened up and specific armor components inside the modules repaired or replaced in the field. In the addition to the composite armor the inside of the hull and the superstructure of the vehicle are fitted with spall panels to minimize the post-armor effects of rounds which penetrate into the vehicle.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment underneath the main gun.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: Like the PzKpfw 151 tank the Ogre is equipped with SDI Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT projectiles. The system consists of a set of pre-warner radar arrays and multiple modular countermeasure modules mounted along the superstructure sides and roof containing electro-optical tracking sensors and directional explosive countermeasures designed to destroy or deflect oncoming projectiles before they strike the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. Six panels are arranged around the sides of the superstructure with another two on the superstructure roof which provide combined 360 degree hemispherical coverage around the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are contained in bricks on the outside of the vehicle and employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) heavy metal tungsten alloy (HMTA) shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the superstructure to provide coverage over the the hull of the vehicle by steering the blast downwards or to defeat over-fly top attack projectiles by firing upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past four or so meters from the vehicle. The countermeasures bricks themselves employ a metal-free composite construction and are encased in a layer of thermoplastic armor to prevent the brick itself from generating any shrapnel and to protect the explosive charges from small arms fire and shrapnel and other hazards. The vehicle by default is fitted with eight countermeasure modules along the sides and front of the superstructure which provide coverage around the the hull and superstructure sides against direct attack or over-fly top-attack projectiles and an additional four roof-mounted countermeasure modules to intercept diving top-attack


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Situational Awareness:
Driver Vision Enhancer:The Ogre features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 12 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The Ogre is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted to the superstructure roof each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions.

Vehicle Missile & Laser Warning Receiver: The vehicle comes equipped with a missile and laser warning system derived from SDI's SN/AAR-64 airborne Missile/Laser Warning System which provides passive warning of incoming threat missiles and illumination by threat lasers. The system employs four optical sensor heads with integral optical signal converters placed around the superstructure of the vehicle with 360 ° azimuth and -10° to + 45° elevation coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which detects lasers in the 0.4-2.1 μm and 8-12 µm wavelength range including laser designators, illuminators, and rangefinders, and a short-wave infrared (SWIR) camera which provides muzzle flash detection detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays.



Communications & Remote Control:
Vehicle Multiband Networking Radio: The primary radio system of the vehicle is an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's superstructure. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.

Remote Control System: For additional safety during minefield breaching operations the Ogre can can remotely teleoperated using a common operator control station (OCS) located inside another manned armored vehicle. In remote control (teleoperation) mode the imagery and navigation data from vehicle's cameras and INS/GPS navigation system are streamed to the operator workstation in near-real time using a LAN 2.4 GHz omni-directional datalink antenna fitted to the vehicle's superstructure. An additional emergency stop radio (ESR) independent of the wireless radio is also included in the communications system which acts as an independent 'kill switch" to trigger system shutdown in teleoperation mode should the vehicle lose contact with the control platform. The operator control station consists of three large multifunction touchscreen displays with bezel buttons for display and crewstation control and a video game console style handheld controller used for remote vehicle control and operation of the vehicle's weapons and engineering equipment. Each multifunction touchscreen displays can be used to display two different information displays including the driving display, control display remote sensor feed, mission planning information, and digital terrain map displays. Video feed from the vehicle's driver vision enhancer (DVE) cameras is streamed at a rate of 1-10 Mbps and displayed in the multifunction displays to remotely drive the vehicle. Below the camera feed are four dials which display the vehicle's current speed, azimuth, pitch, and roll. As a way to prevent the operator from inadvertently flipping the vehicle the pitch and roll dials will flash red if the vehicle's pitch or roll exceeds 30°. The top right of the driver's display is used to display an overhead digital terrain elevation map of the area around the vehicle. The display will also alert the operator if the vehicle's fault detection system detects a fault in the vehicle through a flashing warning at the bottom of the display. The handheld controller is modified from a commercial video game console controller and is used for both driving and for sensor, weapon, and engineering equipment control under teleoperation mode. When driving the vehicle the right joystick is used to steer the vehicle while the left joystick is used to control the vehicle speed. When driving one or both triggers (L1 or L2) must be continuously depressed, ensuring that the vehicle will come to a stop if the operator drops or looses control of the controller.


Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbiology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network.


AI Modules:
To aid in the performance of the crew the vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, and C3 (command, control, and communications).

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 6:41 pm, edited 25 times in total.
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The Technocratic Syndicalists
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Postby The Technocratic Syndicalists » Mon Dec 03, 2018 7:53 am

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Flkpz 502 Orca

General Characteristics:
  • Type: Self-propelled anti-air gun/missile system
  • Weight: 71.7 t
  • Length: 9.8 m
  • Width: 3.8 m
  • Height: 2.8 m
  • Crew: 3 (driver, gunner, commander)
Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI R700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: MG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,300 l (340 Gallon)
  • Operational range: 650 km
Armament:
  • 2x MK50-2/ABM 50 mm chain guns, 1100 rounds
  • 12x RBS 85 hypervelocity surface-to-air missiles
Maneuverability:
  • Power/weight Ratio: 33.5 PS/t (24.6 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.95 kg/cm2
  • Gradient: 70%
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
The Flakpanzer 502 (Flkpz 502) Orca is a mobile air defense vehicle based on SDI's PzKfz 151 Tiger main battle tank chassis. The vehicle replaces the tank turret with an air-defense turret system containing anti-aircraft cannon and missile armament and various radar and electro-optical sensors and is designed to protect combined arms maneuver formations from attack and observation by hostile aircraft, helicopters, UAVs, and RAM (Rocket, Artillery, and Mortar) threats.


Armament
RBS 85 Missile
  • Type: Hyper-velocity surface-to-air missile
  • Length: 2,400 mm
  • Diameter: 160 mm
  • Finspan: 500 mm
  • Weight: 82 kg
  • Speed: 1,700 m/s
  • Altitude (max): 8,000 m
  • Range: 16 km
  • Propulsion: Smokeless dual-pulse solid-fuel rocket
  • Warhead: 12.5 kg directional blast-fragmentation
MK50-2/ABM Cannon
  • Type: Chain gun
  • Weight: 520 kg
  • Length: 4,700 mm
  • Barrel Length: 4,150 mm
  • Width: 450 mm
  • Height: 320 mm
  • Caliber: 50 x 330 mm
  • Rate of fire: Single shot or variable 150-400 RPM
  • Power requirement: 8 kW

Missile Armament:The primary anti-aircraft armament of the vehicle is two retractable missile launchers on either each side of the turret each containing six RBS 85 surface-to-air missiles in individual sealed canisters. After launch the missile is accelerated to a speed of mach 5 (1,700 m/s) using a laser ignited, dual-pulse solid fuel rocket motor employing GAP/HMX/ADN (25.5% Glycidyl Azide Polymer, 4.5% Plasticizer, 58.5% Ammonium Dinitramide, and 11.5% HMX)i insensitive high-energy smokeless propellant. The GAP/HMX/ADN propellant has a higher burning rate and specific impulse than traditional Al/AP/HTPB composite or double base propellant and is completely smokeless, enabling easier tracking of the vehicle's own sensors and proving no visual approach warning to the target. After launch the missile and target are tracked by the vehicle's infra-red and electro-optical tracking sensors and steering instructions are sent to the missile using a CO2 laser which transmits encoded pulses to a rear-facing laser detector on the missile. The missile steers using a combination of four pneumatically actuated tail fins and a jet-vane thrust-vector control (TVC) system and is a capable of up to 70 g overload at ranges up to 12 kilometers. The missile has a range of 500 meters to 16 kilometers and is capable of engaging targets at up to 8,000 meters altitude. The missile contains a 12.5 kilogram directional blast-fragmentation warhead which is detonated either by an electro-optical proximity fuze (for air targets) or an impact fuze (for ground targets or ultra low altitude air targets). The warhead consists of an HMX explosive filled cylinder surrounded by a sleeve of pre-fragmented tungsten shrapnel. The cylinder and fragmentation sleeve surrounded by twelve radial strips of HMX explosive which can each be independently detonated. When the warhead is fuzed the charges facing the strips on the side facing the target are detonated, causes the pre-fragmented case to flatten in the direction of the target. The main charge inside the case and the line charges on the opposite side of the target direction are then detonated, causing the fragments in the flattened part of the case to be ejected in the direction of the target at extremely high velocity.

Cannon Armament:The secondary anti-aricraft armament of the vehicle consists of two SDI MK50-2/ABM automatic cannons which can effectively engage ground and air targets at ranges out to 4 kilometers. The MK50 is a 50mm caliber automatic cannon which fires semi-telescoped 50x330 mm ammunition. The MK50 is an electrically powered chain-gun weapon with a linkless dual-feed ammunition system. Power for the cannon is provided by an 8 kilowatt brushless DC motor which allows for a selectable rate of fire between 150 and 400 rounder per minute. The weapon fires from an open bolt and features absolute hang-fire protection in the form of a mechanical safety interlock system which is de-activates by the recoil force of the cannon. Empty cases are ejected forward through two ejection chutes located underneath and on either side of each barrel. Both the barrel and receiver are chrome-lined for improved service life. The cannons are capable of traversing 360 degrees and elevating from -15 to +85 degrees. The ammunition handling system (AHS) for the cannons consists of twin ammunition transfer units and two linear-linkless magazines each holding 550 cartridges locates on either side of the fighting compartment. The cannon is designed to fire 50x330 mm KETF-T (Kinetic Energy Time Fuze w/ Tracer), a fragmentation round with a programmable fuze which can be set to various airburst, impact, or delay settings. The KETF-T projectile weighs 980 gram is fired at a muzzle velocity of 1,150 m/s. Upon fuzing the round releases 341 spin-stabilized 1.5 gram HMTA (heavy metal tungsten alloy) sub-projectiles in a 15 degree cone ahead of the projectile. A muzzle programming unit containing magnetic flux sensor coils is located at the muzzle end of the cannon which measures the muzzle velocity of each round leaving the barrel and programs the KETF-T round to explode in-flight after a set distance. For engaging armored vehicles the cannon can also fire 50x330 mm APFSDS-T (Armor piercing discarding sabot w/ tracer), an armor-piercing round employing a 640 gram projectile with a depleted uranium staballoy penetrator fired at a muzzle velocity of 1,600 m/s which is capable of penetrating in excess of 180 mm RHA at a range of 1,500 meters. Standard ammunition load for the vehicle is 1000 rounds of KETF-T and 100 rounds of APFSDS-T.


Protection:
Armor Protection:The Orca shares the same base chassis as SDI's Tiger main battle tank and thus features identical hull protection characteristics with the ability to stop 120 and 125 mm APFSDS ammunition and 170 mm diameter HEAT warheads across the frontal 60° arc and 40 mm APFSDS ammunition and 110 mm diameter HEAT warheads across the frontal 180° arc. The turret is constructed from welded >640 BHN ultra-high hardness steel (UHHS) which is designed to provide 360° protection against 15 mm AP ammunition and 155 mm shell fragments. The roof of the features an additional layer of composite armor designed to defeat bomblets and top-attack EFP submunitions and is designed to stop shaped charge warheads up to 70 mm in diameter and EFP warheads up to 150 mm in diameter. Minimization of post-armor effects of both kinetic energy projectiles and shaped charge warheads is achieved through the use of flexible boron-loaded spall panels which are fitted to the inside surfaces of the hull and turret of the vehicle. The spall liner employs multiple layers of orthogonally cross-plied polyethylene fibers which are pressed together into a single layer which is then laminated into a polyethylene resin. The liner serves to reduce the spall cone angle of spall fragments, reducing the spread of fragments inside the vehicle and thus minimizing the chances that a penetrating round will injure or kill the crew. The spall panels are also loaded with 5% by weight boron to provide protection against fast neutron, thermal neutron, primary gamma rays and secondary gamma rays. The bottom and sides of the hull additionally feature a blast-attenuating layer consisting of a vivioelastic foam sandwiched between layers of thermoplastic polyurethane which is placed in between the inner hull plating and spall liner which serves to mitigate the effects of blasts from anti-vehicle mines and IEDs by absorbing and attenuating the blast energy, minimizing vehicle acceleration under blast effects and further increasing crew surviveability.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment underneath the main gun.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: The Orca vehicle is equipped with SDI Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT projectiles. The system consists of a set of pre-warner radar arrays and multiple modular countermeasure modules mounted along the turret sides and roof containing electro-optical tracking sensors and directional explosive countermeasures designed to destroy or deflect oncoming projectiles before they strike the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. Six panels are arranged around the sides of the turret with another two on the turret roof which provide combined 360 degree hemispherical coverage around the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle.

The explosive countermeasures used by the system are contained in bricks on the outside of the vehicle and employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) tungsten-nickel-cobalt (WNiCo) alloy shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the turret to provide coverage over the the hull of the vehicle by steering the blast downwards or to defeat over-fly top attack projectiles by firing upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past 4 or so meters from the vehicle. The countermeasures bricks themselves employ a metal-free composite construction and are encased in a layer of thermoplastic armor to prevent the brick itself from generating any shrapnel and to protect the explosive charges from small arms fire and shrapnel and other hazards. The vehicle by default is fitted with eight countermeasure modules along the sides and front of the turret which provide coverage around the the hull and turret sides against direct attack or over-fly top-attack projectiles and an additional four roof-mounted countermeasure modules to intercept diving top-attack


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Fire Control:
Surveillance & Scanning Radar: The vehicle is equipped with an SDI Sentry-X VSHORAD (Very Short Range Air Defense) radar, an X band (8-10 GHz), digital stacked beam 3D air-surveillance radar which provides three-dimensional, 360° detection, tracking, and target handover of fixed and rotary wing aircraft, missiles and RAM (rocket, artillery, and mortar) targets while on-the-move and in high-clutter and ECM heavy environments. The radar employs an active electronically scanned array (AESA) antenna with air-cooled GaN-on-diamond Tx/Rx elements. The radar has an instrumented range of 75 kilometers and is capable of tracking fighter size targets at 25-30 kilometers and small UAV targets at 10-15 kilometers. Rotation rate of the antenna is 60 rpm and search volume is 360° or in a 40-120° sectors. Elevation coverage is up to 70°. ECCM features of the radar include sidelobe cancellation (SLC), pulse/pulse and burst/burst frequency agility, random PRF switching, and low power frequency modulated continuous wave (FMCW) modes for low probability of intercept/detect (LPD/LPI) operation. An L-band (1 to 2 GHz) Identification Friend or Foe (IFF) antenna is also included in the radar to allow for interrogation of air vehicles. The radar is mounted on an extendable mast and can fold into the vehicle's turret when not in use. The search radar can also detect incoming missiles and will sound an alarm on the operator consoles if the radar detects the launch of an air-to-ground missile.

Fire Control Radar: Targets detected and tracked by the Sentry-X search radar and handed over to the SDI FMG 630 Ku band (15.5 - 17.5 GHz) solid state fire control radar for target engagement while the search radar continues searching for additional target. The FMG 630 radar employs a solid-state Cassegrain antenna connected to a digital receiver and signal processor and transmits with a peak power of 1.5 kW and has a maximum instrumented range of 36 kilometer. The radar is used to align the vehicle's twin 50 mm cannons onto the target and during the engagement and tracks both the target and outgoing rounds to walk them onto the target, terminating the engagement when the radar detects that the target has been killed.

Electro-Optical Gun Targeting System:Visual target identification, surface targeting, and secondary air targeting and fire control for the vehicle's twin 50 mm cannons is provided by a turret mounted, 2-axis stabilized electro-optical targeting system which provides for the observation, tracking, targeting, of both ground and air targets. The system consists of a 3rd generation long wave (LWIR) thermal camera with 1280 x 1024 px resolution and 1.75° to 26°horizontal field of view, color CMOS daylight camera with 1920 x 1080 px resolution and 1.5° to 30°horizontal field of view, eye-safe 2.08 μm Holmium laser rangefinder (LRF), and 1.06 μm Nd:YAG laser designator. A ballistic computer integral to the sight provides for lead-angle computation against moving targets and auto scan / track while scan target auto-tracking capability against moving ground and air targets. The electro-optical gun sensor system is enclosed by a ballistic cover to protect it from shrapnel and small-arms fire and can be elevated from -15° to +85°.

Electro-Optical Missile Fire Control Sensor System: The missile fire control sensor system consists of an 8-12 μm Forward Looking Infra-Red (FLIR) imager with dual field of view with 5° or 15° degrees FOV in azimuth and 4° or 12° FOV in elevation with 4x electronic zoom and a tracking range of 20 kilometers, Daylight CCD camera with 2.4 ° by 1.8° field of view and a tracking range of 15 kilometers, Infrared (IR) tracker with a ±5° FOV, eye-safe 2.08 μm Holmium laser rangefinder (LRF), and a 10.6 μm CO2 guidance laser. Targets detected and tracked by the radar system are automatically passed to the electro-optical fire control sensor system which then passively tracks the target using the FLIR and/or CCD sensors. Distance to the target is determined by the system's laser rangefinder. When the target comes within the effective range of the missile the missile is launched and both the missile and target tracked by the FLIR and CCD sensors. Guidance commands are then sent to the missile using the CO2 guidance laser which provides a guidance beam for the beam-riding missile to steer it towards the target. An additional infrared tracker is used to align the boresight of the CO2 guidance laser with the FLIR and CCD sensors before the missile is captured by the CO2 guidance laser approximately 500 meters after launch. Up to 10 targets can be tracked at once by the electro-optical system while simultaneous guiding up to six missiles to different targets. When not in use the entire electro-optical sensor module can retract inside the turret to protect it from hostile fire.


Situational Awareness:
Driver Vision Enhancer:Like SDU's Tiger main battle tank the Orca features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 14 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The Orca is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted to the turret roof each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions. Each STAS module also contains an imaging sensor autoprocessor (ISA) similar to the one in the gunner and commander FLIR sights which provides automatic target recognition (ATR) capability of threats detected by the system. The STAS can be used to monitor the area around the vehicle during silent watch or while the crew is asleep and includes automatic alert broadcast and target-tracking/moving-target indicator functions which can track detected threats and can interface with the fire control system to hand-off threats to the gunner or commander's sight for immediate engagement by the tank's main or coaxial armament.

Vehicle Missile & Laser Warning Receiver: The vehicle comes equipped with a missile and laser warning system derived from SDI's SN/AAR-64 airborne Missile/Laser Warning System which provides passive warning of incoming threat missiles and illumination by threat lasers. The system employs four optical sensor heads with integral optical signal converters placed around the turret of the vehicle with 360 ° azimuth and -10° to + 45° elevation coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which detects lasers in the 0.4-2.1 μm and 8-12 µm wavelength range including laser designators, illuminators, and rangefinders, and a short-wave infrared (SWIR) camera which provides muzzle flash detection detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays and features integral counterfire capability where the system can automatically slew the turret to within <2 degrees RMS of detected laser or missile threats through a button on the vehicle commander's joystick, presenting the frontal armor of the turret towards the threat and allowing the threat to be rapidly engaged by the tank's armament.

Vehicle Radar Warning Receiver: In addition to the missile and laser warning system the vehicle is fitted with radar warning receivers which warn the crew when the vehicle is being illuminated by a ground or airborne based radar system. The RWR system employs four circularly polarized spiral antennas co-located with the missile/laser warning receiver sensors which provide 360° azimuth and -5° to + 80° elevation detection of RF signals in the 2-40 GHz range. The four antenna feed into two identical receiver connected to a common processor and control unit inside the vehicle. An alphanumeric display and an interface to the vehicle's intercom system provides both visual and audio warning to the crew when the vehicle is being illuminated by a radar including radar type, direction, and scan mode. Like the RWR system is integrated into the vehicle's fire control system and features counterfire capability which automatically slew the turret to within <2 degrees RMS of detected threats through a button on the vehicle commander's joystick.

Acoustic Gunshot Location System: The turret of the vehicle is fitted with an SDI acoustic gunshot location system (AGLS) which uses a series of microphones to triangulate the location of incoming small arms, cannon, and rocket fire. The AGLS uses an array of four microphones fitted to a mast mounted to the rear of the turret which provides 360° hemispherical coverage around the vehicle. Incoming fire is triangulated to a probable shooter location with +/- 2° azimuth, +/-3° elevation, and +/- 10% range RMS error with the ability to interface with the vehicle's GPS system to provide 10 digit grid coordinates of the shooter probable location. The AGLS also interfaces with the vehicle's fire control system and can automatically slew the turret or RWS in the direction of detected threats.


Communications & Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 225 x 225 x 100 mm and weighing 2.75 kg which contains an omindirectional SATCOM antenna which provides two-way L band (1,610.0- 1,660.5 MHz transmit and 1,525-1,559 MHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network. The software component of the Arcturus Battle Management System (ABMS) consists of a series of AI modules run on the system's central processor including navigation aids, situational report and assessment, C3 (command, control, and communications), and target acquisition and engagement modules which provide automatic communication management, sensor control, and target identification and tracking.

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. For example if the system receives an track report than an enemy vehicle(s) are moving along a road it will assume that the vehicle(s) have not detected the presence of own or friendly forces and will keep moving down the road. On the other hand if another track report is received indicating that the enemy vehicle(s) have moved off-road and actively engaging with their armament the system will assume that own or friendly forces have been detected and that the targets will attempt to retreat and form a defilade position. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.

Target Acquisition & Engagement (TA&E): The Target Acquisition & Engagement or TA&E module is responsible for generating and updating track files of enemy contacts and disseminating them to the other AI modules and advising the vehicle commander on recommended actions in repose to enemy contacts. The TA&E module takes input from the vehicle's radar and electro-optical sensors and generates track reports of each contact including type (tank, helicopter, APC), position (GPS grid coordinates and elevation), heading (degrees), moving (yes/no), activity, and sensors used. Different vehicle sensors are used to fill out the different parts of the contact report, ie the automatic target recognition (ATR) capability of the dual band FLIR sights are used for determining contact type while the laser rangefinder and far target locator (FTL) system are used to fill in contact position and heading. After a track report has been generated the module then determines the kill probability (the probability the own vehicle can successfully engage and defeat the contact with its own weapons) and the contact danger (the probability the contact will detect and engage the own vehicle) based on contact type and position, own vehicle position, and environmental factors including terrain and ambient weather conditions. Contact danger will also be judged as extreme if the vehicle's missile, laser, and radar warning sensors indicate the vehicle is being actively illuminated or shot at. In response to extreme danger contacts the module will automatically deploy smoke grenades in the threat direction and prompt the crew to immediately move and engage the threat with the vehicle's weaponry. If the contact threat is judged as less severe the module can run various simulations to evaluate possible engagement scenarios and provide a recommended engagement option which could be to engage the contact with the vehicles weapons, continue monitoring the contact with the vehicle's sensors, or to simply ignore it.
Last edited by The Technocratic Syndicalists on Sun May 01, 2022 12:09 pm, edited 33 times in total.
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The Technocratic Syndicalists
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Postby The Technocratic Syndicalists » Sat Dec 08, 2018 12:14 pm

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BgPz 151 Minotaur

General Characteristics:
  • Type: Armored recovery vehicle
  • Weight: 63.5 t
  • Length (hull): 10.6 m
  • Width: 3.8 m
  • Height: 3.6 m
  • Crew: 3 (driver, operator, commander)

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: Active in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 65 km/h
  • Fuel capacity: 1,250 l (330 Gallon)
  • Operational range: 550 km

Performance:
  • Crane Capacity: 40 t
  • Winch capacity: 120 t
  • Towed load: 90 t
  • Earth working capacity: 300 m3/h

Armament:
  • 1x 40mm GMG, 96 rounds
  • 1x 8 mm MG 45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 34.6 PS/t (25.2 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.95 kg/cm2
  • Gradient: 70% m
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
The Bergepanzer 151 (BgPz 151) Minotaur is a armored recovery vehicle variant of the PzKpfw 151 Tiger main battle tank designed by SDI Vehicle Systems. The vehicle consists of a modified PzKpfw 151 Tiger chassis with an additional superstructure, high-tensile winches, and a powered, extensible crane and is designed for recovering damaged, overturned or stuck tracked vehicles along with performing additional maintenance tasks, earthmoving, and clearing obstacles.


Armament:
Scanfire Dual RWS: For protection against close in threats the vehicle is fitted with an SDI Scanfire Dual remotely operated weapon station mounted to the superstructure roof which includes an MG 45E machine gun, 40 mm GMG and electro-optical sensor suite. The Scanfire Dual weighs 280 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with both an automatic grenade launcher with 96 rounds of 40 x 53 mm ammunition and an MG 45E machine gun with 1,000 rounds of 8x57 mm ammunition. The Scanfire Dual features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. The weapon station includes dual-axis gyro-stabilization to allow for effective fire while the vehicle is moving. The weapon station is traversed and elevated using brushless DC servomotors and features -15 to +70 degrees elevation and 360 degrees of traverse. The sensor system includes a CCD daylight camera with up to 10x magnification, an uncooled 640 x 480 pixel LWIR (long wave infrared) imager, and an eye-safe Nd:YAG laser rangefinder.

Smoke-grenade launchers:For obscuration purposes the vehicle is equipped with a total 24 smoke grenade launchers grouped into six groups of four on the front superstructure face covering the front two 90 degree sectors. The smoke launchers fire 66mm diamater red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. .The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each frontal 90 degree sector.


Recovery & Engineering Equipment:
For towing, winching and recovery operations the BgPz 151 is fitted with a crane, several main and auxiliary winches, and tow bar along with other assorted repair and maintenance equipment. The vehicle's crane is mounted to a rotary platform on the right side of the hull which can traverse 270° and can be extended 10 meters with a maximum 40,000 kg lifting capacity. The crane is used to remove the turrets or powerpacks of main battle tanks and other armored fighting vehicles and for other lifting tasks. The vehicle has two 60,000 kgf capacity winches (120,000 kgf with additional pulley blocks) each with 200 meters of cable along with an auxiliary winch with a 6,500 kgf capacity and 280 meters of cable. All three winches are located inside the armored superstructure behind the crew compartment. The vehicle also carries two 40,000 kg hydraulic jacks, an electric arc welding system, air compressor, an electric hand-held circular saw, and various tracked vehicle tools for field repairs. The rear of the vehicle can also carry a spare PzKpfw 151 powerpack for rapid field replacement using the vehicle's crane.

For winching, earthmoving and obstacle clearing operations the Minotaur is fitted as standard with a straight dozer blade which attaches to front of the vehicle using the Hydraulic Equipment Adaptor (HEA) attached to the glacis of the vehicle. The pitch of the blade is adjustable via a series of pitch cylinders and is used to anchor the vehicle into the ground for winching operations and can also be used to fill trenches, clear rubble and other obstacles, and dig defensive emplacements with the ability to excavate 300 m³ of earth per hour. The blade is 3.5 meters wide and 1.2 meters tall and is constructed from high tensile low carbon steel with a lower cutting edge constructed from hardened tool steel. The dozer blade is also heavily armored and is designed to withstand mine damage. The blade controlled by either the driver or commander using a joystick with three pre-set operation positions including stowed, deployed, and float


Protection:
Armor Protection:The BgPz 151 Minotaur employs the same heavy-metal composite armor system as fitted to the PzKpfw 151 main battle tank which is designed to provide protection against kinetic energy (KE) threats in the form of long-rod penetrators fired by high-pressure tank cannons and chemical energy (CE) threats including large-caliber shaped charge munitions. The composite armor covers the front and sides of the the hull and superstructure with the remainder of the vehicle protected only by conventional steel armor. The line-of-sight (LOS) thickness of the armor of the vehicle measures 1,300 mm meters across the glacis and superstructure front and 700 mm across the superstructure sides. The armor is designed to provide frontal /- 30° protection against large caliber tank gun fired APFSDS rounds (800-1000 mm RHA penetration) and large caliber anti-tank guided missiles (~170mm diameter SC with 1500-1600 mm RHA penetration) and 360° protection against 15mm AP ammunition and handheld anti-tank weapons (110mm diameter SC). Appropriate average RHA equivalent protection for the glacis and superstructure armor across the frontal 60 degree arc is 1,000-1,200 mm RHA against kinetic-energy munitions and 1,800-2,200 mm versus chemical-energy munitions. In the addition to the composite armor the inside of the hull and the superstructure of the vehicle are fitted with spall panels to minimize the post-armor effects of rounds which penetrate into the vehicle.

Fire extinguishing system: The crew, fuel, and powertrain compartments of the vehicle include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment underneath the main gun.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.



Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Situational Awareness:
Driver Vision Enhancer:The vehicle features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 12 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the vehicle while under hatch. The STAS system consists of four camera modules mounted to the corners of the hull each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions.

Vehicle Missile & Laser Warning Receiver: The vehicle comes equipped with a missile and laser warning system derived from SDI's SN/AAR-64 airborne Missile/Laser Warning System which provides passive warning of incoming threat missiles and illumination by threat lasers. The system employs four optical sensor heads with integral optical signal converters placed around the superstructure of the vehicle with 360 ° azimuth and -10° to + 45° elevation coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which detects lasers in the 0.4-2.1 μm and 8-12 µm wavelength range including laser designators, illuminators, and rangefinders, and a short-wave infrared (SWIR) camera which provides muzzle flash detection detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays.


Communications & Remote Control:
Vehicle Multiband Networking Radio: The primary radio system of the vehicle is an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's superstructure. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.


Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbiology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network.


AI Modules:
To aid in the performance of the crew the vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, and C3 (command, control, and communications).

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.
Last edited by The Technocratic Syndicalists on Tue Nov 16, 2021 4:35 pm, edited 21 times in total.
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Postby The Technocratic Syndicalists » Wed Jan 01, 2020 10:25 am

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HTTS 50.1000 10x10

General Characteristics:
  • Type: 10x10 heavy tactical truck
  • Curb weight: 22,000 kg
  • Payload weight: 28,000 kg
  • Gross vehicle weight: 50,000 kg
  • Length: 11.7 m
  • Width: 2.5 m
  • Height: 3.2 m
  • Crew: 2+1

Mobility:
  • Engine: AMG HL80 turbocharged V8 diesel, 735 kW (1,000 PS)
  • Transmission: Diesel-electric hybrid transmission; 735 kW AC generator, 10x 100 kW hub motors
  • Energy storage: 28 kW-h lithium-ion battery pack
  • Suspension: Hydropneumatic
  • Brakes: Disc brakes with ABS (Anti-Lock Braking System)
  • Tires: 10 (+1) 16R20 with run-flats and CTIS (Central Tire Inflation system)
  • Steering: individual wheel and skid steering
  • Max road speed: 110 km/h
  • Fuel capacity: 700 l
  • Operational range: 1,000 km
  • Ground clearance: 0.60 m

Armament (optional):
  • SDI Scanfire RWS, 1x 8 mm MG 45E (1,000 rounds)

Maneuverability:
  • Gradient: 70%
  • Side slope: 40%
  • Fording Depth: 1.5 m
  • Trench Crossing: 2.5 m
  • Vertical Wall Climb: 0.6 m


Overview
The HTTS 50.1000 10x10 is a family of high-mobility 10x10 diesel-electric trucks designed by SDI Vehicle Systems. The HTTS 50.1250 10x10 is the largest truck in the SDI HTTS series of vehicles and is available is various variants including load handling, recovery vehicle, and heavy equipment transporter versions which share a common chassis, drivetrain, and crew cabin.


Mobility
  • Name: HL80
  • Type: Multi-fuel diesel engine
  • Length: 1,080 mm
  • Width: 700 mm
  • Height: 760 mm
  • Dry Weight: 830 kg
  • Bore/stroke: 115/107 mm
  • Displacement, cylinder: 1.00 l
  • Displacement, total: 8.00 l
  • Charging method: Twin variable-geometry turbochargers
  • Intercooling: Air-water aftercooler
  • Number of Cylinders: 8, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 210 g/kW-hr
  • Power: 735 kW (1,000 PS) @ 4,250 RPM
  • Torque: 2,050 N-m (1520 ft-ib) @ 3,800 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The SDI 10x10 HTTS uses a diesel-electric series hybrid propulsion system with power from a 1,000 PS (735 kW) AMG (Arkaenisch Motorenfabrik Gesellschaft) HL110 V10 turbodiesel engine used to drive a 920 kW, 240 VAC generator which in turn powers ten 600 VDC, 135 PS (100 kW) hub motors which drive each wheel through a synchronized two-speed gearbox integrated with the electric motor into each wheel hub. Energy storage is provided through the use of twin floor mounted battery pack banks each containing ten 24V, 23 kW battery packs with a combined capacity of 28 kW-h at a nominal bank voltage of 220 V. The battery is charged by the engine and using regenerative braking and when fully charged gives the vehicle an all-electric range of 30 km at a speed of 30 km/h. This system eliminates the mechanical connection between the diesel engine and the drive axles and thus eliminates the need for a torque converter, transmission, transfer case, and drive shaft. The use of regenerative braking, energy storage, and the ability of the diesel engine to run at a constant RPM independent of the wheel speed also results in a roughly 20% fuel savings over a conventional drivetrain. The diesel-electric hybrid drive has four modes of operation; hybrid (HEV), electric transmission (ET), electric vehicle (EV), and Auxiliary Power (AP). Hybrid mode is the default mode and uses the battery to supplement the diesel engine power during acceleration, absorb energy during regenerative braking, and soften engine transients. Electric transmission mode is used when the battery is depleted, disconnected, or damaged and operates without the battery as a conventional diesel-electric transmission. Electric vehicle operates with the diesel engine off and is used for silent mobility or silent watch purposes to minimize the signature of the vehicle. Auxiliary power mode is used to configure the system to provide up to 730 kW of 60 Hz, 240 VAC export power which can be used to run an airfields, weapons or radar systems, field hospitals, or command centers.

The AMG HL80 engine which powers the vehicle is an 8 cylinder, multi-fuel, dual overhead camshaft, twin sequentially turbocharged, liquid cooled V engine developing 1,000 PS of power at its maximum rated speed of 4,250 rpm. The engine direct-drives a 735 kW 3-phase synchronous generator which provides electrical power to the traction motors driving each wheel of the vehicle. The HL80 employs a common rail fuel-injection system with a fuel rail running the length of the engine and twin hydraulic boost pumps running at up to 3,100 rpm to pressurize the fuel to 1,800 bar for injection into each cylinder. Turbocharging is accomplished with twin single-stage variable-geometry turbocharger units using variable-area turbine nozzles which providing boost pressure ratios up to 5:1. A water-to-air charge-air cooler is placed after the turbocharger compressor stages to cool and density the air before entering the combustion chambers. To maximize engine performance across a broad ambient temperature spectrum the water and oil cooling system of the engine are split into a high temperature loop which cools the piston liners, cylinder heads, and other engine components along with the first stage of the charge-air cooler, and a low temperature loop which cools the power electronics, engine oil, and the second stage of the charge-air cooler. A dual-circuit water pump circulates cooling water through both the high and low temperature loops and then through the radiator cooling system which employs twin 65 kilowatt variable-speed fans to cool the coolant before it's passed into the expansion tank and then circulated again through the twin coolant loops. A 170 kW electric flywheel starter-generator is used to start the engine to provides 600 VDC power to the twin 65 kW radiator fan motors and 20 kW of 24 VDC power the vehicle cabin for the vehicle power-supply system. In addition to the HL80 engine the HTTS also includes a 10 kw auxiliary power unit (APU) which provides 60 Hz, 240 volts alternating current (VAC) at a design operating speed of 3,600 rpm. The APU is a 4 cylinder, 4 stroke water-cooled diesel engine brushless permanent magnetic AC generator and is used to power the vehicle's HVAC and environmental control systems system, NBC system, and other electronics while the main engine is off.

The HTTS 50.1000 10x10 is driven by ten SDI designed permanent magnet synchronous motor (PMSM) hub motors each rated at 100 kW maximum and 65 kW continuous power which are integrated along with a two-speed (plus neutral) planetary reduction gearbox and a liquid cooled disc brake into a hub drive unit (HDU) which is contained in each wheel hub. Power for each HDU is provided by a pair of generator converter boxes (GCBs) which convert 3-phase AC power from the vehicle's 3-phase synchronous generator to 600 VDC direct current which is then distributed to the drivetrain using twin DC busbars running along either side of the vehicle frame to each hub drive unit. Cooling for each HDU is provided a cooling circuit inside the drive unit which supplies 16 liters per minute (LPM) of 80°C propylene glycol (PGW) coolant to cool each drive unit.

The HTTS 50.1000 10x10 is constructed from a stiffened torsion-resistant box frame with C-section longitudinal members and welded tubular cross members formed from Ultra-high-strength steels (UHSS) with a yield strength exceeding 980 MPa. The vehicle employs variable-height semi-active hydro-pneumatic independent suspension with each wheel being mounted to trailing arm connected to the chassis which contains the hydro-pneumatic suspension mechanism. Vehicle steering is done with a 'steer-by-wire' system which combines wheel steer and skid steer; using conventional Ackermann steering at high speeds and using skid steering (like a tracked vehicle) at lower speeds which is achieved via differential speed between wheels on either side of the vehicle. Using its hub motor drive the vehicle can also pivot turn in place. The tires used in the vehicle are 1600R 20 with run-flat inserts. A central tire inflation system (CTIS) is fitted, having four predetermined terrain settings (Highway, Cross-Country, Mud & Snow, Emergency) and a Run Flat (RF) mode which regularly checks tire pressures and inflates as needed to compensate for leaks. A spare wheel and tire is mounted behind and above the crew cab.


Load Handling System :
The HTTS is equipped with an SDI Intelligent Load Handling System (ILHS) which allows for the automated loading and unloading of ISO containers and various flatrack modules weighing up to 25 tonnes onto the HTTS from within the confines of the truck cabin.


Flatrack Modules:
Flatrack Refueling Module: The Flatrack Refueling Module (FRM) system is a self contained fuel module that provides the ability to transport, filter and distribute fuel to vehicles and aircraft in expeditionary environments. The FRM is mounted to a modified ISO container frame and contains a baffled stainless steel fuel tank with a capacity of 10,000 liters, a 1,000 liters per minute flow rate diesel engine driven centrifugal pump, a backup 200 liter per minute flow rate positive displacement electrical pump, filter separator, two hoses with refueling nozzles, aviation fuel test kits, fire extinguishers, grounding rods, and a digital flow meter. The FRM is capable of fueling and defueling kerosene-based one aircraft or fueling two ground vehicles simultaneously. The FRM measures 6.0 x 2.6 x 2.4 meters and weighs 7,000 kilograms empty and 15,500 kilograms with a full fuel load.

Tank Rack Modules: The Tank Rack Module (TRM) is a fuel tank module which along with the Pump Rack Module forms SDI's Modular Fuel Farm System (MFFS) which consists of 14 Tank Rack Modules and two Pump Rack Modules. The TRM consists of a baffled stainless steel fuel tank with a capacity of 13,500 liters and a 75 liter per minute electric pump. The TRM measures 6.0 x 2.6 x 2.4 meters and weighs 3,800 kilograms empty and 15,300 kilograms with a full fuel load.

Pump Rack Module: The Pump Rack Module (PRM) consists of a fuel pump and filtration system with a 2,500 liters per minute flow rate diesel engine driven centrifugal pump, filter separator, and 1,000 meters of hose. Two Pump Rack Modules along with 14 Tank Rack Modules form SDI's Modular Fuel Farm System (MFFS) which is used to provide air forces and mechanized ground forces with a rapidly emplaced fuel distribution system which can rapidly receive, store and distribute fuel to ground vehicles, helicopters, and fixed wing aircraft.

Water Tank Module: The Flatrack Water Tank Module (WTM) is a water tank module designed to distribute drinking water to forward units. The WTM consists of a 7,500 liter stainless steel potable water tank, a diesel engine driven 200 liter per minute flow rate pump, filling stand, and 20 meter hose reel. The FRM measures 6.0 x 2.6 x 2.4 meters and weighs 12,000 kilograms when fully filled.

Firefighting Module: The Firefighting Module (FFM) is a water tank module designed to for firefighting. The FFM consists of a 11,500 liter stainless steel non-potable water tank, a 600 liter firefighting agent tank, a diesel engine driven 2,500 liter per minute flow rate pump, a 100 liter fuel tank, a water cannon capable of spraying over 12 meters to either side of the vehicle, and 15 meters of 38 mm diameter fire hose. The FFM measures 6.0 x 2.6 x 2.4 meters and weighs 2,400 kilograms empty and 13,800 kilograms when fully filled.

Repair Station Module: The Repair Station Module (RSM) is a dismountable maintenance and repair module which is intended to act as a mobile maintenance shop for armored units. The RSM mounted to a modified ISO container frame and contains a 2.2 x 2.2 x 2.3 meter workshop shelter, 70 kW diesel generator providing 400 VAC 50 Hz electrical power, 1.2 MPa electric air compressor with a 1,400 liter per minute flow rate and 300 liter capacity, welding cabinet with SMAW and MIG welders, a 360° crane which can lift up to 7 tonnes to a height of 5 meters at a radius of up to 4 meters, a deployable shelter with a canvas tarp to provide additional working area whle being protected from the weather, and over 700 assorted tools. The entire FRSM measures 6.0 x 2.6 x 2.4 meters and weighs 12,000 kg when fully loaded with equipment.

Dump Bed Module: The DBM converts the vehicle into a dump truck and consists of a dump truck bed mounted to a modified ISO container frame. The dump bed is constructed from 7.5mm thick abrasion-resistant steel and has a capacity of 10.7 cubic meters. The bed can be elevated to 50° using twin hydraulic actuators supplied by a 25 MPa, 115 liter per minute hydraulic system. The DBM measures 6.0 x 2.4 x 2.1 meters and weighs 4,800 kilograms empty and 16,500 kilogams when fully loaded with bituminous material.

Floating Bridge Modules: The Floating Bridge Modules (FBMs) are part of SDI's Foldable Floating Bridge (FFB) system, a floating pontoon bridge system consisting of floating bridge modules which can be connected together to form a floating bridge for tracked and wheeled vehicles. The Floating Bridge Modules (FBMs) come in Ramp Module and Interior Module versions, each of which consists of a four-pontoon folding module with two interconnected inner and outer pontoons which unfold automatically when the bridge module is released into the water. The Interior Modules are designed act as the primary load bearing competent of the floating bridge and consists of two inner roadway pontoons and two outer bow pontoons. The inner pontoons feature two watertight compartments and have a roadway welded to them while the two outer pontoons aid in flotation and provide additional roadway space for two lane traffic along with walkways for personnel on either side of the roadway. The Interior Modules are connected to each other by engaging four upper couplings on the outer pontoons followed by two lock pins on the inner pontoons. The lock pins act as bearing points between consecutively joined bays, allowing the entire bridge to hinge with the weight of a moving vehicle and with water currents or uneven water conditions. The Ramp Modules are designed to be used at either end of a floating bridge are are similar in construction to the interior modules with the exception that the inner and outer pontoons are tapered toward the shore end of the module. The shore end of the ramp module contains a 2.5 meter long ramp actuated by a hydraulic system inside the module which allows the ramp to be raised to accommodate bank heights of up to 2.35 meters. The Ramp Module also contains two lockable, self-draining stowage boxes contained in the outer pontoons. When folded each module is 7.0 meters long, 3.3 meters wide, 2.35 meters tall, and weighs 6,350 kg. When unfolded each module is 7.0 meters long, 8.6 meters wide and 1.3 meters tall. The Foldable Floating Bridge can be deployed in rivers with a water speed of up to 3.15 m/s features a total usable road width of 6.75 meters for two lane traffic with vehicles weighing up to 20 tonnes and 4.5 meters for single lane traffic with vehicles weighing up to 80 tonnes. Creating a 100 meter long bridge takes approximately 45 minutes and requires 13 Interior Modules and 2 Ramp Modules
while creating a 25 meter takes approximately 15 minutes and requires 2 Interior Modules and 2 Ramp Modules.


Armament:
Scanfire RWS: The self-defense purposes the roof of the HTSS can be optionally fitted with an SDI Scanfire remotely operated weapon station. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers.

Smoke-grenade launchers: The HTTS can optionally be equipped with a total 16 smoke grenade launchers grouped into two sets of 4-tube launchers on either side of the cab roof which cover the forward two 90º sectors. The smoke launchers fire 66mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The launchers are controlled manually from a panel in the crew cabin which can fire individual grenades or salvos of four across each forward 90 degree sector.


Protection:
Armor protection: The HTTS features a fully armored cab constructed from welded 5 mm 600 BHN hardness ultra-high-hardness steel (UHHS) plates with integral silicon carbide (SiC) ceramic/polyethylene (UHMWPE) composite armor panels, ballistic glass windows, and an inner M5 fiber/epoxy composite spall liner which provides 360º azimuth and 0 - 30°elevation protection against 7.62 mm tungsten core armor piercing ammunition at a distance of 30 meters and 155 mm high explosive shell fragments at 60 meters. Under body protection for the crew cab consists of a multi-layered internal V-hull with a kevlar floor lining and mine blast protective crew seats which is designed to withstand a 10 kg TNT equivalent explosive blast AT Mine denoting under center or an 8 kg TNT equivalent explosive mass AT Mine detonating under one of the wheel wells.

Fire extinguishing system: The crew cab, fuel tanks, and powertrain compartments of the HTTS include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew cab are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the floor of the crew cab which through a series of hoses and pipes spray Halon agent into the crew compartment when the system detects a fire. The system can also be manually activated through a panel near the driver's seat. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew cab and maintains cab pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing absorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Sensors & Electronics:
Panoramic Driver Vision Enhancer: For driving at night or in low-light level conditions the cab of the HTTS is fitted with a SDI Panoramic Driver Vision Enhancer (PDVE) module which contains three 640 x 512 pixel 17 µm uncooled vanadium oxide (Vox) microbolometer sensors operating in the LWIR band (8-12µm) which combined provide a stitched 140° horizontal by 30° vertical field of view ahead of the vehicle. HDMI output from the panoramic DVE sensor is streamed at 30 Hz to an 800 x 600 pixel resolution driver’s vision enhancer (DVE) display & control module located on the vehicle dashboard which allows the driver to pan the entire 140° field of view with the DVE output scaled to the full display size.

Vehicle Multiband Networking Radio: For C4I and communications purposes the HTTS vehicle is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.

Integrated Driver Assist System: The HTTS comes standard fitted with SDI's Integrated Driver Assist System (IDAS) system which includes forward collision warning (FCW), emergency brake assist (EBA), adaptive cruise control (ACC), lane departure warning (LDW), electronic stability control (ESC), and blind spot monitoring functions.

Forward collision warning (FCW) and emergency brake assist (EBA): The forward collision warning (FCW) and emergency brake assist (EBA) system employs a front facing 77 GHz millimeter wave (MMW) radar in the front bumper which is intended to detect moving and stationary vehicles or pedestrians in the vehicle's path. The system will then generate both audible and visual warnings and if necessary will automatically brake and de-throttle the engine if the driver does not react in time. Should the driver apply the brakes with insufficient force a dynamic brake support (DBS) system will increase the brake force above what the driver has applied in order to avoid a collision.

Adaptive cruise control (ACC): The adaptive cruise control (ACC) system employs the forward facing 77 GHz MMW radar along with a 24 GHz ground speed radar mounted with a 35° look down behind the forward wheel well and automatically adjusts the vehicle speed to maintain a safe distance from vehicles ahead on the road. The adaptive cruise control system is controlled by a lever attached to the steering column. Gently tapping the lever either up or down engages the adaptive cruise control and increases the cruise speed by one kilometer per hour. Pushing or depressing the lever further increases or decreases speed by five kilometres per hour. A knob on the lever is used to adjust following distance in one meter increments which is displayed on the central screen in front of the driver. Pushing the lever forward, braking, or accelerating will disable the adaptive cruise control.

Lane departure warning (LDW): The lane departure warning (LDW) system employs two sets of CCD cameras on either side of the crew cab which track the lane markings on either side of the vehicle and provide both an audible and visual warning to the driver when one of the lane markings is crossed without the turn signal being applied.

Electronic stability control (ESC): The electronic stability control (ESC) system is designed to mitigate severe oversteer or understeer conditions leading to vehicle loss of-control (LOC) as well as mitigating on-road rollovers by using a lateral acceleration sensor, yaw rate sensor, and steering wheel angle sensor to monitor the vehicle’s directional control and selectively applying the brakes at each wheel position and reducing engine power in order to help the driver regain control of the vehicle. The ESC will also maintain heading control by determining the driver’s intended heading via the speed and steering wheel angle sensors and automatically adjusting the steering behavior of the vehicle if the steering response does not match the driver’s intention.

Blind spot monitoring: The blind spot monitoring system employs two side looking 24 GHz short-range radars mounted either side of the crew cab with a 160° field of view which will generate a visual warnings for the driver when the radars detect the presence of cars or pedestrians located in one of the vehicle's blind spots. The system will generate an additional audible warning if the driver activates the turn signal while the system has detected an object in one of the vehicle's blind sports and will increase the resistance in the steering wheel if a driver attempts to change lanes while the system has detected an obstacle in one of the blind spots.

Autonomous Navigation System: In addition to the Integrated Driver Assist System the HTTS is fitted with SDI's autonomous navigation system (ANS) which permits fully autonomous on and off-road self-driving along with robotic convoy operations. The autonomous navigation system (ANS) includes terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. For detecting terrain and obstacles in front of the vehicle the ANS employs twin laser imaging perception modules (LIPMs) mounted on top of the crew cab which each contain a 2-D scanning LADAR (LAser Detection And Ranging) sensor and two pairs of stereo color and infrared cameras. The LADAR sensors operate with a 905 nm wavelength at 75 Hz with 0.25°angular resolution and generate a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. Each LADAR sensor is augmented by a set of stereo camera pairs which use twin 1024 x 768 pixel CCD cameras and twin 320 x 240 pixel uncooled LWIR (8-12 μm) cameras with 90° FOV lenses which provide stereo range acquisition of terrain obstacles ahead of the vehicle and when combined with the LADAR sensors provides 3D imagery of terrain in the direction of travel.

The LADAR and stereo camera sensors along with ten wheel encoders, ten vehicle height management sensors HMS, a ground speed radar, and a forward looking 77 GHz millimeter wave (MMW) radar are coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer and a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation.

The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.

The autonomous navigation system of the vehicle can follow two different modes; autonomous mode and vehicle leader-follower mode. In autonomous mode the user selects one or more GPS waypoints using the control display which the vehicle will then drive to while autonomously detecting and avoiding any obstacles along the route. In vehicle leader-follower or “robotic convoy" mode the vehicle can be instructed to follow either a manned vehicle or another unmanned robotic convoy vehicle which it will attempt to follow at a specified distance using it's forward imaging perception sensors. Should the follower vehicle lose track of the 'leader' vehicle the follower will revert to GPS navigation using GPS waypoints received by the leader vehicle.


Variants

HTTS LHS: The HTTS Load Handling System or HTTS-LHS (Arcaenian designation: LKW 25t MULTI) is the base variant of the HTTS family and is intended to be a general-purpose cargo vehicle capable of hauling ammunition, flatracks, ISO containers, tactical bridging and support equipment, engineering equipment, and fuel containers. The HTTS-LHS features an integral Intelligent Load Handling System (ILHS) which allows for the automated loading and unloading of ISO containers and various flatrack modules weighing up to 25 tonnes onto the HTTS from within the confines of the truck cabin. The system is controlled by a single operator using a computer-assisted user interface located in the passenger seat of the truck cabin. The HTTS-LHS can additionally tow a three axle trailer which can accommodate an additional flatrack, ISO container, or up to 25 tonnes of payload.

HTTS Recovery Vehicle: The HTTS Recovery Vehicle or HTTS-RV (Arcaenian designation: Bergefahrzeug 41 (BFz 41) ) performs heavy wrecker and recovery missions including the recovery of damaged, immobilized, swamped, stuck, or overturned vehicles included wheeled or tracked vehicles weighing up to a maximum of 50,000 kg. The HTTS-RV has an empty weight of 36,000 kg and a curb weight of 48,000 kg and features a three-section 360° rotatable boom extendable to 12.5 meters from the vehicle. The boom is powered by two 250 kN winches and can lift over 35,000 kg at a 6 meter radius from the vehicle with a maximum lifting capacity of 50,000 kg and can be remotely operated from within or outside of the vehicle. The HTTS-RV additionally features twin 250 kN constant-pull drag winches with 100 meters of rope along with four outriggers and one large hydraulic spade mounted at the rear to stabilize the vehicle during craning and winching operations. The vehicle also has an 8 kN pulling auxiliary winch in addition to the two 250 250 kN main winches. Damaged vehicles up to 50,000 kg can be towed in a suspended semi-lifted position behind the vehicle on paved roads.

HTTS Heavy Equipment Transporter: The HTTS Heavy Equipment Transporter or HTTS-HET (Arcaenian designation: Schwerlasttransporter 85t (SLT 85t)) is a prime mover variant of the HTTS designed to be used as a tank transporter and to tow self-propelled artillery systems, construction materials, and other heavy military loads over long distances and across rough terrain. The HTTS-HET is intended to be used with an 8-axle, 64 wheel semi-low loader with hydraulic steering and suspension which can accommodate payloads up to 85,000 kg in weight and includes a two-piece loading ramp which is hydraulically operated. The HTTS-HET chassis additionally features twin 250 kN winches and a third 15 kN auxiliary winch. Maximum Gross Combined Weight Rating (GCWR) of the HTTS-HET is 140,000 kg and maximum on-road speed is 80 kph.

HTTS All Terrain Crane: The HTTS All Terrain Crane or HTTS-ATC (Arcaenian designation: Fahrzeugkrane schwere (FKS)) is a self-propelled crane variant of the HTTS which features a rotating superstructure containing a crew cab and a crane with a 60 meter telescoping hydraulic boom and a maximum lifting capacity of 130 tonnes. The crane has a 6 sections telescoping boom made from St 130 ultra-high-strength structural steel with one base section and and five telescoping sections extended using a single hydraulic cylinder which allows the crane to be extended from 12.8 meters to 60.0 meters long. The crane is powered by a three circuit hydraulic system with a double axial piston pump driven by a 4.8 liter four-cylinder AMG diesel engine in the superstructure with a rated power of 175 PS (130 kW) at 2,000 RPM. The crane is controlled electronically by a crane operator inside the superstructure cabin with twin joystick levers for simultaneous operation of crane motions. The chassis of the vehicle includes a total of four 4-point, double telescopic hydraulic outriggers with an outrigger base 7.5 m x 8.0 m. The HTTS-ATC has a curb weight of 60,000 kg (including a 6,300 kg counterweight).
Last edited by The Technocratic Syndicalists on Sat Jul 16, 2022 6:41 pm, edited 52 times in total.
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The Technocratic Syndicalists
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Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Fri Jul 03, 2020 12:04 pm

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AKpfw 504 Riptide

General Characteristics:
  • Type: Amphibious assault vehicle
  • Weight: 34.5 t
  • Length: 9.0 m
  • Width: 3.6 m
  • Height: 3.0 m
  • Crew: 3 (driver, gunner, commander) + 16 dismounts

Mobility:
  • Engine: AMG HL425 multi-fuel quad-turbo V12 diesel engine, 2,200 kW (3,000 PS)
  • Water drive: 2x 60 cm water jets, 100 kN thrust each
  • Transmission: AMG AK 7-900 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: Retractable in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max water speed: 50 km/h (27 knots)
  • Fuel capacity: 1,500 l
  • Operational range: 550 km land, 120 km @ 25 knots water

Armament:
  • 1x MK50 50 mm chain gun, 300 rounds
  • 2x twin-tube ATGM launchers, 8x RBS 94 Lance Hypervelocity ATGMs
  • 1x 8 mm MG-45, 2,000 rounds
  • 1x 40mm GMG-40, 240 rounds

Maneuverability:
  • Power/weight Ratio: 86.9 PS/t (63.8 kW/t)
  • Ground clearance: 0.50 m
  • Gradient: 70%
  • Sideslope: 40%
  • Trench crossing: 2.4 m
  • Vertical wall climb: 1.0 m


Overview:
The Amphibienkampfwagen 504 (AKpfw504) Riptide is a high-speed amphibious assault vehicle designed by SDI Vehicle Systems. Designed with high water speeds in mind the Riptide features a unique composite space-frame construction and a high-power diesel engine combined with twin waterjet thrusters and a hydroplaning hull designs enabling the vehicle to reach water speeds in excess of 25 knots.


Design:
The Riptide features a unique planing hull designed for high water speeds with a large moveable bow plane at the front and large folding transom flap at the rear of the hull. When the vehicle enters the water the bow plane and transom flap are lowered and the running gear retracted into the hull and covered with a series of chine flaps, giving the vehicle a more hydrodynamic profile which lets it plane over the water's surface at speeds over 25 knots. The vehicle also contains a total of five bilge pumps, three hydraulic and two electric, which are capable of removing up to 1,500 liters of water per minute from the vehicle while it is as sea. When the vehicle reaches the shore the tracks are deployed and the bow and transom flaps are raised and the vehicle transitions into land mode. The vehicle is operated by a crew of three with the driver, commander, and gunner sitting side-by-side at the front of the vehicle with the driver and commander provided with hatches with built in observation periscopes. Behind the crew compartment is the longitudinally mounted 3,000 PS V12 diesel engine which for balance reasons is located in the middle of the vehicle with intakes and exhausts located on the roof. The transmission of the vehicle is located at the front of the hull in just ahead of the the crew stations and transfers engine power to the two sprockets on either of the hull. Behind the engine is the crew compartment which can accommodate up to 16 soldiers in folding seats on either side of the vehicle or up to 3,700 kg of cargo. Above the crew compartment is located the vehicle's remote turret which contains a 50mm cannon, coaxial machine gun, and anti-tank missile launchers. At the rear of the troop compartment is hydraulically-powered rectangular door used for exiting and entering the vehicle. Two additional sliding hatches are also located on the roof on either side of the troop compartment. On either side of the rear door are the vehicle's two waterjet thrusters which are connected using two drive shafts on either side of the hull to a power-take off assembly mounted to the transmission at the front of the vehicle. Each waterjet additionally contains an armored cover which folds down over the waterjet exhaust nozzle when the vehicle transitions into land mode.


Armament:
SDI MK50 Cannon
  • Type: Chain gun
  • Weight: 520 kg
  • Length: 4,700 mm
  • Barrel Length: 4,150 mm
  • Width: 450 mm
  • Height: 320 mm
  • Caliber: 50 x 330 mm
  • Shell: 50 x 228 mm
  • Rate of fire: Single shot, or variable 150-400 RPM
  • Power requirement: 6 kW
RBS 94 Lance
  • Type: Hypervelocity ATGM
  • Length: 1,300 mm
  • Diameter: 152 mm
  • Weight: 50 kg
  • Speed: 2,400 m/s
  • Range: 10 km
  • Propulsion: dual-pulse solid-fuel rocket
  • Warhead: 4 kg DU alloy penetrator

Cannon Armament: The primary armament of the Riptide is the SDI MK50, a 50mm caliber electrically driven linkless dual-feed automatic cannon which is located in an unmanned, fully stabilized turret at the rear of the vehicle. The turret uses electric turret drives and can traverse a full 360º at up to 45°/s and elevate from -10º to +45º at 45°/s with < 0.3 mrad pointing accuracy in both traverse and elevation. The MK50 is an electrically powered chain-gun weapon firing from an open-bolt with a linkless dual-feed ammunition system. Power for the cannon is provided by an 8 kilowatt brushless DC motor which allows for a selectable rate of fire between 150 and 400 rounds per minute. Empty cases are ejected forward through two ejection chutes located underneath and on either side of the barrel. Both the barrel and receiver are chrome-lined for improved service life. An additional rectangular stiffening sleeve with cooling vent cutouts is attached to the barrel to improve accuracy during fully automatic fire on the high rate-of-fire setting. 150 rounds of 50 x 330 mm ammunition are stored ready to use in the turret in two 75 round boxes with another 150 50mm rounds stowed inside the hull. For firing programmable air-burst munition rounds the 50mm cannon features a muzzle programming unit containing magnetic flux sensor coils which measures the muzzle velocity of each round leaving the barrel and programs the round to explode in-flight after a set distance. Standard ammunition is either 50x330mm APFSDS-T (Armor piercing discarding sabot w/ tracer), an armor-piercing round employing a depleted uranium staballoy penetrator capable of penetrating in excess of 180 mm RHA at 1,500 meters, and PABM-T (Programmable airbust munition w/ tracer), a HE-fragmentation round with a programmable fuze which can be set to various airburst, impact, or delay settings.

Secondary Armament: An 8mm MG-45E machine gun is mounted coaxial to the main armament with 1,000 rounds stored ready to fire in the turret and another 1,000 rounds stored in the hull. The turret of the vehicle additionally includes an SDI GMG-40 40mm grenade-machine gun (GMG) mounted to an MSSA (main sensor slaved armament) remote weapon station attached to commander's independent thermal sight (CITS) on top of the turret. The SDI GMG-40 is short-recoil operated, belt fed automatic grenade launcher capable of firing high velocity 40mm programmable air-burst grenades out to an effective range of 1,500 meters. The weapon station includes a box containing a 48 round belt ready to fire with another 192 rounds of 40mm ammunition stored in the hull.

Missile Armament: To combat main-battle tanks and other heavy vehicle threats the Riptide is equipped with twin turret mounted missile launchers containing two RBS 94 Lance missiles each. The RBS 94 Lance is a hyper-velocity anti-tank guided missile (HVATGM) which features a dual-pulse solid fuel rocket which accelerates the missile at over 1,000 gs to to a burnout velocity of mach 7 at sea level. The missile employs side-scatter laser beam riding guidance system which uses the vehicle's FLIR and 1.06-μm laser designator to deliver guidance updates to the missile in flight. In addition to the four missiles stored ready to fire in the turret the vehicle carries another four missiles in the hull as reloads.

Smoke-grenade launchers: The vehicle is equipped with a total 24 smoke grenade launchers in two retractable 12-tube launchers in the bustle which cover the forward two 90 degree sectors. The smoke launchers fire 66mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each forward 90 degree sector.


Protection:
Passive Armor:The vehicle employs a fiberglass-epoxy composite hull with embedded ceramic armor which designed to provide frontal 60 degree arc protection against 30mm APFSDS rounds fired at 1,000 meters and 360 degree protection against 15mm AP ammunition fired at 500 meters at 155 shell fragments at 10 meters. The armor also covers the vehicle's roof where it provides protection against shaped charge bomblets up to 70 mm in diameter and EFP warheads up to 150 mm in diameter. The armor consists of an outer S2 fiberglass phenolic layer for fire, smoke, and toxicity (FST) protection, an outer structural layer of S-2 fiberglas-epoxy composite, and a layer of hexagonal silicon carbide (SiC) tiles 10 cm wide and 2 cm thick glued to an EPDM rubber backing layer, inner S-2 fiberglass hull structural layer, and a phenolic polymer inner layer glued to the inside of the hull acting as a spall liner. Total thickness of the armor is 40mm, increasing to 60mm across the front of the hull where two layers of ceramic tiles are used to provide additional ballistic protection. The armor panels are molded using vacuum assisted resin transfer molding (VARTM) into top and bottom composite armor halves which are then bolted to an internal space-frame structure made from welded 2519-T87 aluminum alloy which provides the hull with its torsional rigidity and is where the running gear and powertrain assemblies are bolted to. Further protection for the crew is provided by an armored titanium crew capsule placed between the front mounted transmission and center mounted engine.

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppresion system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the crew compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere. An additional 2.5 kg Halon fire extinguisher is also stored in the fighting compartment.


Mobility:
  • Name: HL435
  • Type: Multi-fuel diesel engine
  • Length: 1,820 mm
  • Width: 1,410 mm
  • Height: 1,080 mm
  • Dry Weight: 3,300 kg
  • Bore/stroke: 160/176 mm
  • Displacement, cylinder: 3.54 l
  • Displacement, total: 42.5 l
  • Compression ratio: 13.5
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 12, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 210 g/kW-hr
  • Power: 2,200 kW (3,000 PS) @ 2,400 RPM
  • Torque: 9,000 N-m @ 2,400 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel

Engine: The vehicle is powered by an AMG HL435 quad-turbo V12 diesel engine with a maximum power output of 3,000 PS at 2,400 RPM on water and 1,000 PS at 2,100 RPM on land. The HL435 is a four-stroke, direct injection diesel engine with 12 cylinders arranged in a 90°degree V configuration. The engine is water cooled and employs a dry-sump lubrication system. For forced air induction the HL435 engine is equipped with four turbo-charging systems each consisting of a two stage in-line sequential turbocharger with variable turbine nozzles and an air-to-coolant intercooler and aftercooler. Fuel injection in each cylinder is via a CRS (Common Rail System) electronically controlled common-rail fuel injection system with two high-pressure fuel injection pumps operating at 1800 bar. The HL435 is fitted with a nuclear and EMP hardened digital engine control module which controls fuel injection, monitors and controls fuel-air ratio in each cylinder to prevent smoke emissions, modulates engine power as a function of ambient temperature and radiator capacity, and provides monitoring of engine RPM, and oil and coolant pressure temperature, and flow rates.

Water jets: For water operations the vehicle is equipped with two 60 cm diameter counter-rotating waterjet thrusters located at the rear of the hull on either side of the rear exit ramp. Each waterjet thruster consists of a flush inlet mounted along the hull bottom, single stage rotor, stator, and exit nozzle with jet deflectors providing steering and thrust reversal capability. Each waterjet thruster is rated at 1,400 PS of shaft horsepower and moves in excess of 3,000 liters of water per second providing a maximum water thrust of approximately 100 kilonewtons. The twin waterjet thrusters are capable of accelerating the vehicle in water from a standstill to hydroplaning speed in less than 30 seconds and give the vehicle a maximum water speed in excess of 25 knots at up to sea state 3 (1.25 meter high waves).

Transmission: The vehicle is equipped with an AMG AK 7-900 hydrokinetic transmission located at the front of the hull which provides range control, steering, braking, and power take-off functions and delivers engine power to either the tracks and/or waterjet thrusters for sea and land operations. The transmission contains a hydrostatic steer unit with an infinitely variable steering range, integral hydraulic brake, a torque converter with an automatic lockup clutch connected to a seven speed planetary range pack with 7 forward and 3 reverse gears, a two-speed power take-off module with water jet clutch which is used to transfer engine power to the two waterjet thrusters for sea operations. The transmission is capable of operating in three modes; water mode which transfers up to 3,000 PS at 2,400 RPM to both waterjet thrusters with the tracks disconnected from the transmission, transition mode which delivers up to 1,800 PS at 2,100 RPM to both the waterjets and tracks, and land mode which delivers up to 1,000 PS at 2,100 RPM to the tracks only with the waterjet drives disconnected from the transmission.


Suspension & Running Gear:
Suspension:The suspension system used by the vehicle is an SDI designed semi-active in-arm hydro-pneumatic suspension system with seven 610 mm diameter rubber-tired road wheels on either side of the chassis each mounted on a retractable swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. When the vehicle is in the water the swing arms are retracted into the hull and the road wheels and tracks covered by hydraulically actuated chine flaps on either side of the hull to minimze hydrodynamic drag. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydromechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The suspension also allows the vehicle to "tilt" forwards or backwards permitting additional gun elevation and depression.

Running gear: The vehicle features a decoupled running gear design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle's road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units. Instead of conventional steel tracks the vehicle employs composite rubber band tracks which are 50% lighter and result in a 70% vibration reduction and 10 dB noise reduction inside the vehicle at a road speed of 50 kph. The tracks are 600 mm wide with a 120 mm pitch with a designed durability of over 5,000 km before replacing.


Sensors & Electronics
Gunner's Sight: The vehicle is equipped with a two-axis stabilized stabilized gunner's thermal sight which is housed in an armored titanium covering on the left side of the vehicle's remote turret. The main features of the sight are a third generation dual-wavelength (3-5 um and 8-14 um) thermal imager and high-resolution color CCD imager with 2-axis independently stabilized line of sight, ballistic computer, eye-safe laser rangefinder, and integrated GPS/inertial navigation system. The third generation thermal imager used with the gunner's sight is a 1280 x 1024 pixel dual color (MWIR and LWIR) capable Mercury cadmium telluride (HgCdTe) staring focal plane array (FPA) detector based system which features an architecture common to several other SDI designed third gen thermal imaging systems. The thermal imager is cooled using a Stirling cycle linear drive cryocooler which cools the detector assembly to 77 degrees K. The detector and crycooler system are contained in a single Standard Advanced Dewar Assembly (SADA), a closed-cycle dewar-cooler assembly containing the linear crycooler, infrared FPA, Dewar, and various control electronics and sensors. The dual-color thermal imager features a color fusion system which assigns colors to pixel values from each MWIR and LWIR band (red for LWIR, cyan for MWIR), adding color contrast to the otherwise black-and-white thermal image. The thermal sight can be toggled between 3x magnification wide field of view (WFOV), 10x magnification medium field of view (MFOV), x25 narrow field-of view (NFOV), and x50 ultra-narrow field of view settings. Mounted alongside the thermal imager is a 1920 x 1080 pixel visible/near IR monochrome CCD camera with selectable 10x NFOV and 3x MFOV optical magnification with additional x25 narrow and x50 ultra-narrow magnification digital zoom capability which provides the gunner's sight with an additional daylight channel in addition to the dual-band thermal channel. An image fusion function is also available combines the data from the dual-band thermal imager and the CCD camera to provide a fused image selectable on the sight control panel from 100% visible / 0% IR to 0% visible / 100% IR in infinitely variable increments. Range information for the fire-control system is provided by a 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder which provides range data accurate to 1 meter from ranges of 80 meters up to 20 kilometers. The sight additionally contains a 1064 nm laser designator, laser illuminator and laser spot tracker. The sight's dual axis stabilized head mirror assembly provides for enhanced on-the-move (OTM) stabilization capability, ensuring the reticle of the sight stays stabilized in the center of the sight while the vehicle is on the move. Dual-axis stabilization is provided by micromachined 2-axis hemispherical Resonator Gyroscopes (HRGs) with 0.001 deg/hour drift capability integrated into the sights inertial measurement unit (IMU) system.

The gunner's sight is further integrated with a GPS/INS navigation system which inputs accurate heading, attitude, velocity and position information of the vehicle into the sight's ballistic computer. The navigation system combines 3 axis fibre optic gyroscopes, 3 axis pendulous accelerometers, and digital magnetic compass with further sensor input from vehicle motion sensor (VMS) systems in the drivetrain and two lightweight, jam resistant DGPS antenna integrated into either side of the sight housing. Attitude information from the GPS is used to give the sight far target location (FTL) capability which combines data from the GPS/INS system and laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The ballistic computer for the gunner's sight is contained in a single line replaceable unit (LRU) and features a shock, radiation, and electro- static discharge hardened outer casing and a convection cooling system with-50 to +70 degree C operating capability. The ballistic computer synthesizes inputs from multiple sensors including laser rangefinder, barrel temperature sensors and dynamic muzzle reference system (MRS), RFID propellant temperature sensors, vehicle motion sensors (VMS), and inertial navigation vehicle position sensors to give the gunner an accurate firing solution which maximizes probably of first-round hit out to ranges of several kilometers against moving and stationary targets while the tank is stationary or traversing across both smooth or rough terrain.

The gunner's sight features an automatic target recognition (ATR) capability imaging through an SDI designed imaging sensor autoprocessor (ISA) unit built into each sight. The ISA employs parallel very high speed integrated circuit (VHSIC) processors operating at 10 billions of operations per seconds (BOPS) contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the sight's dual-band FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, and other armored vehicles. The output from the sight is displayed in the gunner's binocular image control unit (BICU), a dual binocular display mounted in the gunner's station which generates a stabilized virtual image of the output of the sighting unit. The display from the gunner's sight is also displayed in the gunner's primary sight extension (GPSE) in the commander's station which allows the commander to see what the gunner is looking at and to potential override him or sight and fire the cannon if necessary.

Commander's Sight: External vision for the commander is provided by the commander's independent thermal sight (CITS) which features the same infrared imager, color CCD camera, laser range finder as the gunner's sight. The CITS features independent dual-axis HRG stabilization along with servomotor actuated 360 degree azimuth and -30 to +70 degree elevation travel. Like the gunner's sight the CITS is contained within an armored housing which protects the assembly against shrapnel and small arms fire. The CITS additionally includes track-while-scan capability and an integral ballistic computer and ATR processor identical to the one in the gunner's sight which enables lead angle computation capability and far-target location ability like that of the gunner's sight. The CITS features both manual and automatic scan settings and an additional gun line of sight (GLOS) mode where the remote turret is slaved to the CITS, allowing the commander to accurately aim and fire the vehicle's cannon and missile armament using the CITS. High Definition video output from the CITS is transferred into the turret via a 100 MHz bandwidth fiber-optical slip ring and displayed on the commander's integrated display (CID), a 1920 x 1080 resolution touchscreen SXGA display with 20 programmable edge keys all with variable backlight which can each be assigned to various surveillance or fire control functions.

Driver Vision Enhancer: The vehicle features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 14 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55 x 40 degree field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: For enhanced situational warns the vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the tank while under hatch. The STAS system consists of four camera modules mounted on the corners of the hull each containing two 640×480 pixel long-wave infrared (8-14µm) thermal imagers and two ultra-high resolution color CMOS daylight CCD cameras set a 90 degree angle from each other. The four sensor modules provide overlapping 360 degree horizontal field-of-view and -30 to +45 degree vertical field-of-view day and night vision around the vehicle The STAS is capable of detecting a person sized target out to 300 meters (900 meters with the daylight channel) and includes automatic alert broadcast and target-tracking/moving-target indicator functions and can interface with the fire control system to hand-off threats to the gunner or commander's sight for immediate engagement by the tank's main or coaxial armament.

Missile/Laser Warning System: The vehicle is equipped with a passive missile and laser warning system which provides both warning of incoming threat missiles and illumination by threat lasers. The system employs five optical sensor heads with integral optical signal converters mounted around the turret which provide combined 360 degree azimuth coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which warns the crew when the aircraft is being illuminated by a laser designator/illuminator/rangefinder or if the aircraft is being targeted by a laser beam-riding missile, and a short-wave infrared (SWIR) camera which provide detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through the vehicle's intercom system and onboard situational awareness displays. The system is also integrated into the vehicle's fire control system and features integral counterfire capability where the system can automatically slew the turret to within <2 degrees RMS of detected laser or missile threats through a button on the vehicle commander's joystick to allow the threat to be rapidly engaged by the vehicle's armament.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:09 pm, edited 27 times in total.
SDI AG
Arcaenian Military Factbook
Task Force Atlas
International Freedom Coalition


OOC: Call me Techno for Short
IC: The Kingdom of Arcaenia

User avatar
The Technocratic Syndicalists
Minister
 
Posts: 2173
Founded: May 27, 2015
Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Thu Aug 27, 2020 10:33 am

Image

AKpfw 903 Marauder

General Characteristics:
  • Type: Amphibious IFV/reconnaissance vehicle
  • Weight: 32.0 t
  • Length: 7.9 m
  • Width: 3.0 m
  • Height: 2.3 m (hull)
  • Crew: 3 (driver, gunner, commander) + 8 dismounts

Mobility:
  • Engine: AMG HL220 multi-fuel twin-turbo V12 diesel engine, 610 kW (830 PS)
  • Water drive: 2x shrouded propellers, 13.5 kN thrust each
  • Transmission: AMG 7S320 (7 forward, 1 reverse gears)
  • Suspension: Independent hydropneumatic
  • Max road speed: 110 km/h
  • Max water speed: 13.5 km/h
  • Fuel capacity: 560 l
  • Operational range: 1,100 km land, 70 km water

Armament:
  • 1x MK50 50 mm chain gun, 300 rounds
  • 2x twin-tube ATGM launchers, 8x RBS 94 Lance Hypervelocity ATGMs
  • 1x coaxial 8 mm MG-45, 2,000 rounds
  • 1x RWS mounted 40mm GMG-40, 240 rounds

Maneuverability:
  • Power/weight Ratio: 25.6 PS/t (18.8 kW/t)
  • Ground clearance: 0.50 m
  • Gradient: 70%
  • Sideslope: 40%
  • Fording depth: 1.2 m
  • Trench crossing: 2.0 m
  • Vertical wall climb: 0.8 m


Overview:
The Amphibienkampfwagen 903 (AKpfw 903) Marauder is an amphibious 8x8 armored fighting vehicle designed by SDI Vehicle Systems.


Armament
SDI MK50 Cannon
  • Type: Chain gun
  • Weight: 520 kg
  • Length: 4,700 mm
  • Barrel Length: 4,150 mm
  • Width: 450 mm
  • Height: 320 mm
  • Caliber: 50 x 330 mm
  • Rate of fire: Single shot or variable 150-400 RPM
  • Power requirement: 6 kW
BGM-194 Lance
  • Type: Hypervelocity ATGM
  • Length: 1,300 mm
  • Diameter: 170 mm
  • Weight: 50 kg
  • Speed: 2,400 m/s
  • Range: 10 km
  • Propulsion: dual-pulse solid-fuel rocket
  • Warhead: 5 kg DU alloy penetrator

Cannon Armament: The primary armament of the vehicle is the SDI MK50, a 50mm caliber electrically driven linkless dual-feed automatic cannon which is located in an unmanned, fully stabilized turret at the rear of the vehicle. The turret uses electric turret drives and can traverse a full 360º at up to 45°/s and elevate from -10º to +45º at 45°/s with < 0.3 mrad pointing accuracy in both traverse and elevations. The MK50 is an electrically powered chain-gun weapon firing from an open-bolt with a linkless dual-feed ammunition system. Power for the cannon is provided by an 8 kilowatt brushless DC motor which allows for a selectable rate of fire between 150 and 400 rounds per minute. Empty cases are ejected forward through two ejection chutes located underneath and on either side of the barrel. Both the barrel and receiver are chrome-lined for improved service life. An additional rectangular stiffening sleeve with cooling vent cutouts is attached to the barrel to improve accuracy during fully automatic fire on the high rate-of-fire setting. 150 rounds of 50 x 330 mm ammunition are stored ready to use in the turret in two 75 round boxes with another 150 50mm rounds stowed inside the hull. For firing programmable air-burst munition rounds the 50mm cannon features a muzzle programming unit containing magnetic flux sensor coils which measures the muzzle velocity of each round leaving the barrel and programs the round to explode in-flight after a set distance. Standard ammunition is either 50 x 330mm APFSDS-T (Armor piercing discarding sabot w/ tracer), an armor-piercing round employing a depleted uranium staballoy penetrator capable of penetrating in excess of 180 mm RHA at 1,500 meters, and PABM-T (Programmable airbust munition w/ tracer), a HE-fragmentation round with a programmable fuze which can be set to various airburst, impact, or delay settings.

Secondary Armament: An 8mm MG 45E machine gun is mounted coaxial to the main armament with 1,000 rounds stored ready to fire in the turret and another 1,000 rounds stored in the hull. The turret of the vehicle additionally includes an SDI GMG 97 40mm grenade-machine gun (GMG) mounted to a remote weapon station attached to commander's sight on top of the turret. The SDI GMG 97 is short-recoil operated, belt fed automatic grenade launcher capable of firing high velocity 40mm programmable air-burst grenades out to an effective range of 1,500 meters. The weapon station includes a box containing a 48 round belt ready to fire with another 192 rounds of 40mm ammunition stored in the hull.

Missile Armament: To combat main-battle tanks and other heavy vehicle threats the Goliath is equipped with twin turret mounted missile launchers containing two RBS 94 Lance missiles each. The RBS 94 Lance is a hyper-velocity anti-tank guided missile (HVATGM) which features a dual-pulse solid fuel rocket which accelerates the missile at over 1,000 gs to to a burnout velocity of over mach 6 at sea level. The missile employs side-scatter laser beam riding guidance system which uses the vehicle's FLIR and 1.06-μm laser designator to deliver guidance updates to the missile in flight. In addition to the four missiles stored ready to fire in the turret the vehicle carries another four missiles in the hull as reloads.

Smoke-grenade launchers: The vehicle is equipped with a total 16 smoke grenade launchers grouped into two sets of 4-tube launchers on either side of the turret face which cover the forward two 90º sectors. The smoke launchers fire 76 mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual (0.4 to 0.7 µm) and infrared (0.7 to 14 µm) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. Each smoke grenade weighs 1.2 kg including 800 grams of red phosphorous fill and is launched to a range of 40-45 meters where the grenade bursts and produces a smokescreen approximately 12 meters long and 6 meters high for a duration of 20-30 seconds. The launchers can also fire fragmentation grenades containing an explosive charge and 750 grams of steel balls which are designed to burst at a height of 5-6 meters above the ground. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launches smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. The launchers can also be controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each 90° sector.

Flare mortars: Mounted to the turret of the vehicle are four 71 mm flare mortars which are designed to fire infrared flares designed to provide near-infrared wavelength illumination of target areas at night or during low-visibility weather conditions for dismounted infantry units equipped with night vision goggles. The four flare mortars are divided into two groups of two mortars each with each pair having a control unit with firing buttons inside the crew compartment and a connection cable which is connected to the vehicle's 24V DC electrical bus. Each mortar has a fiberglass barrel approximately 91 centimeters long and fires a 34 centimeter long flare massing 1.2 kg at a muzzle velocity of around 147 m/s. The barrel can be elevated from 0°to +45° in 5° steps with the launcher having three preset ranges of 450, 950, and 1,600 meters. Each flare consists of a front segment containing an electrical time fuse, pyrotechnic charge, separating charge and infrared spectral flare, rear segment with a parachute, and a tail section which contains stabilization fins and the propellant charge. The time fuze triggers the separating charge which causes the munitions front and rear segments to split and release the infrared flare along with the parachute assembly which is ejected by a spring in the rear projectile segment. The flare then ignites and burns for around 30 seconds as it descends towards the ground at a rate of around 3 m/s. The flare provides illumination in the 0.7-1.2 µm region and illuminates a ground area around 1,500 meters in diameter. Four flares are carried in the four turret mounted mortars with another eight normally stored inside the crew compartment.


Protection:
Armor:The Marauder employs a welded ultra high hardness steel (UHHS) monocoque construction which provides 360° protection from 7.62 mm AP ammo at a range of 30 meters and 155mm shell fragments at a range of 60 meters. The base protections is augmented by bolted-on applique armor panels consisting of hot-isostatic-pressed (HIP) silicon carbide (SiC) tiles embedded in a forged 7075 aluminum alloy matrix. This armor raises the vehicle protection level of the vehicle to frontal 60° arc protection against 30 mm APFSDS rounds fired at 1,000 meters and 360° protection against 15mm AP ammunition fired at 100 meters and 155 mm high explosive shell fragments at 10 meters. The inside of the vehicle is also fitted with a spall liner consisting of multiple layers of orthogonally cross-plied M5 ballistic fibers laminated into a flexible thermoplastic resin. The spall liner serves to reduce the spall cone angle of spall fragments, reducing the spread of fragments inside the vehicle and thus minimizing the chances that a penetrating round will injure or kill the crew. Underbelly protection consists of a V-hull design with underbelly armor designed to resist blasts of up to 10 kg TNT under the vehicle.

Fire extinguishing system: The crew, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the crew compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously online begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.

Active Protection System: The Marauder is equipped with SDI's Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT and APFSDS projectiles. The system consists of a set of pre-warner radar arrays and multiple hybrid protection modules mounted along the front, sides, and rear of the hull consisting of embedded electro-optical tracking sensors and directional explosive countermeasures which are encased in a layer of ceramic armor which provides protection for the system components and acts as additional passive armor for the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels mounted around the vehicle on the outside of the APS modules which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radar are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) tungsten-nickel-cobalt (WNiCo) alloy shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the hull to have overlapping coverage over the the entire hull of the vehicle by steering the blast side to side and downwards or to defeat over-fly top attack munitions by steering the blast upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past 4 or so meters from the vehicle. To protect the APS modules from shell fragments, small arms fire, and other sources of damage and to absord the residual debris from projectiles intercepted by the system the sensors and explosive countermeasure are encased in a layer of encapsulated ceramic armor rated to stop 14.5mm AP at 20 meters and 152/155 mm high explosive shell fragments at 30 meters. The system is capable of intercepting four simultaneous threats and with a reaction time of 0.5 milliseconds is capable of intercepting RPGs or other munitions launched from within 10 meters of the vehicle.


Mobility:
  • Name: HL220
  • Type: Multi-fuel diesel engine
  • Length: 1,430 mm
  • Width: 1,210 mm
  • Height: 1,100 mm
  • Dry Weight: 1,250 kg
  • Bore/stroke: 130/140 mm
  • Displacement, cylinder: 1.825 l
  • Displacement, total: 21.9 l
  • Compression ratio: 14.5
  • Charging method: Twin variable-geometry turbochargers
  • Intercooling: Air-water aftercooler
  • Number of Cylinders: 12, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 200 g/kW-hr
  • Power: 610 kW (830 PS) @ 2,100 RPM
  • Torque: 3,200 N-m @ 1,500 RPM
  • Fuel: Ultra-low sulfur diesel
Engine: The Marauder is powered by an AMG HL220 V12 turbo-diesel engine with a maximum power output of 610 kW (830 PS) at 2,100 RPM. The HL220 is based on a civilian truck engine which has had its oil system, turbocharger, and intercooler modified to increase the engine's torque and power output. The HL220 engine crankcase is made from an aluminum block with a thin, thin, low-friction iron-carbon alloy coatings applied to the cylinder walls to reduce piston friction. The forged crankshaft is supported by 10 bearings and employs a balancing system with counter rotating weights sized and aligned to minimize shaft vibrations. The engine pistons are made from steel and employ a stepped-lip combustion cavity design while the cylinder heads are constructed from a cast aluminum-silicon alloy and are fitted with double water jackets for improved cooling. Fuel injection is via an electronically controlled common rail system which injects fuel at 2050 bar into each engine cylinder. The forced air induction system of the engine employs two variable turbine geometry (VTG) turbochargers which are controlled electronically by a regular which varies engine boost pressure as a function of engine exhaust pressure and temperature. Each turbocharger assembly consists of a turbine wheel, compressor wheel, and bearing housing. Boost pressure is adjusted by varying a series of adjustable guide vanes in front of the turbine wheel which open or close to vary the pressure seen by the turbine wheel. To minimize exhaust emissions the HL160 engine features a multistage exhaust gas recirculation (EGR) system which reduces the amount of nitrous oxide (NOx) in the exhaust. The EGR system employs a high-pressure circuit which take portion of the exhaust gas from the exhaust manifold and pass it through a exhaust-coolant heat exchanger before feeding it in into the intake manifold. An electronically controlled valve adjusts the amount of re circulation in the high-pressure circuit as a function of exhaust temperature and pressure, intake pressure, and engine load and RPM. An additional low-pressure EGR circuit takes exhaust downstream of the catalytic converter and passed it through an additional exhaust-coolant heat exchanger and injects into the inlet manifold downstream of the high-pressure EGR circuit.

Propellers & Amphibious Drive: The vehicle's amphibious drive consists of two hydraulically powered counter-rotating propellers located on each side at the rear of the vehicle driven by power take-off (PTO) from the vehicle's transmission. Each propeller produces up to 13.5 kN of thrust and can drive the vehicle in water forwards up to 13.5 km/h and reverse up to 7 km/h at up to sea state 3 (1.25 meter wave height). Additional amphibious systems include a snorkel, a retractable front breakwater, and two electric bilge pumps with capacity of 380 litres/min each and two hydraulic bilge pumps with a capacity of 435 litres/min each.

Transmission: The engine is connected to an AMG 7S320 automatic transmission with seven forward and one reverse gears. The 7S320 is a modified heavy duty truck transmission which has been adapted for the Marauder 8x8 drivetrain. The 7S320 itself is 1,020mm long, 370mm wide and tall, and weighs 550 kg. The 7S320 employs four planetary gearsets and six hydraulic clutches to achieve seven gear ranges with an 11.92 overall gear ratio spread. Gear ratios are 7.63 (first), 3.51 (second), 1.91 (third), 1.43 (fourth), 1.00 (fifth), 0.74 (sixth), 0.64 (seventh), and -4.8 (reverse). The transmission also includes a hydraulic power take-off (PTO) which is used to drive the vehicle's propellers when in the water.

Drivetrain: The Marauder's 8x8 drive systems uses a single-differential twin-shaft design with a transversal differential lock and 1st, 2nd, and 4th axle steering. The Marauder employs eight off-road run-flat tires with a diameter of 1,332 mm, width of 435 mm, and a maximum rated load of 5,600 kg. The tires are each fitted with a VFI (Variable Function Insert) run-flat insert which allows the vehicle to travel up to 30 km at speeds up to 50 km/h in the event of a flat. A central tire inflation system (CTIS) is fitted as standard and lets the driver adjust the pressure in each individual tire as necessary to improve traction performance over different terrain and includes four terrain settings (Highway, Cross-Country, Mud & Snow, Emergency) and a Run Flat (RF) mode which checks tire pressures regularly and inflates as needed to compensate for leaks. Braking is via pneumatic anti-lock braking system (ABS) with disk brakes fitted to each wheel. Suspension is hydro-pneumatic and fully independent on each wheel station which allows the driver to adjust the ride height and tilt the vehicle during loading and unloading operations.
Last edited by The Technocratic Syndicalists on Thu Mar 23, 2023 6:39 pm, edited 27 times in total.
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The Technocratic Syndicalists
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Postby The Technocratic Syndicalists » Wed Oct 28, 2020 7:16 pm

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GdW 30 Lynx

General Characteristics:
  • Type: Light tactical vehicle
  • Curb weight: 6,200 kg
  • Gross vehicle weight: 9,000 kg
  • Length: 5.4 m
  • Width: 2.1 m
  • Height: 2.0 m
  • Crew: 2

Mobility:
  • Engine: AMG HL32 turbocharged inline 6-cylinder diesel, 225 kW (305 PS)
  • Electric Motor: 160 kW (215 PS) permanent magnet motor (PMM)
  • Transmission: Parallel Hybrid-Electric drive, AMG 9S70 (9 forward, 1 reverse gears), 2-speed transfer case
  • Suspension: Independent double wishbone
  • Max road speed: 130 km/h
  • Fuel capacity: 300 l
  • Operational range: 900 km

Armament (optional):
  • 1x 8 mm MG 45E (1,000 rounds)

Maneuverability:
  • Power/weight Ratio: 49.2 PS/t (36.3 kW/t)
  • Ground clearance: 0.50 m
  • Gradient: 60%
  • Sideslope: 40%
  • Fording Depth: 1.5 m
  • Trench crossing: 0.75 m
  • Vertical wall climb: 0.5 m


Overview:
The Geländewagen 30 (GdW 30) Lynx is a 4x4 tactical vehicle designed by SDI Vehicle Systems. The Lynx is available in multiple variants including the base utility vehicle as well as command and control (C2) and ambulance variants sharing a common chassis.


Armament:
Scanfire RWS: The self-defense purposes the roof of the Lynx can be optionally fitted with an SDI Scanfire remotely operated weapon station. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers.


Protection:
The Lynx features a fully armored cab constructed from welded 5mm 600 BHN hardness ultra-high-hardness steel (UHHS) plates with integral silicon carbide (SiC) ceramic/polyethylene (UHMWPE) armor panels, ballistic glass windows, and an inner M5 fiber/epoxy composite spall liner which provides 360º protection against 7.62 mm armor piercing ammunition at a distance of 30 meters and 155 mm high explosive shell fragments at 60 meters. Under body protection consists of a multi-layered internal V-hull with a kevlar floor lining and mine blast protective crew seats which is designed to withstand a 10 kg TNT equivalent explosive blast AT Mine denoting under center or an 8 kg TNT equivalent explosive mass AT Mine detonating under one of the wheel cells.


Mobility:
  • Name: HL32
  • Type: Multi-fuel diesel engine
  • Length: 1,100 mm
  • Width: 810 mm
  • Height: 570 mm
  • Dry Weight: 280 kg
  • Bore/stroke: 85/94 mm
  • Displacement, cylinder: 0.53 l
  • Displacement, total: 3.2 l
  • Compression ratio: 22.0:1
  • Charging method: Two-stage variable-geometry turbocharger
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 6 in-line
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 205 g/kW-hr
  • Power: 225 kW (305 PS) @ 4,100 RPM
  • Torque: 680 N-m @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Lynx employs a parallel hybrid-electric drivetrain which combines a three-phase brushless permanent magnet electric motor and mid-mounted 3.2L turbodiesel engine. The HL32 is an in-line 6 cylinder, four stroke, water cooled, sequentially turbocharged diesel engine with a common rail fuel injection system with a maximum power output of 300 PS at its rated speed of 4,100 RPM.. The 2-stage turbocharger employs a low and high pressure compressor driven by a single exhaust turbine with an air-water intercooler in between the compressor stages and an air-water aftercooler after the high pressure stage. The HL32 has an operating temperature range of -32 °C to +49 °C and is multi-fuel capable with the ability to run on both diesel fuel and aviation kerosene fuel. The vehicle carries 300 liters of fuel onboard which gives a road range of approximately 900 kilometres. The HL32 engine is coupled to an AMG 9S70 nine-speed automatic transmission with 9 forward and 1 reverse gears. The 9S70 uses four planetary gearsets and six hydraulic clutches to achieve nine gear ranges with a 9.84:1 overall gear ratio spread. Gear ratios are 4.71 (first), 2.85 (second), 1.91 (third), 1.38 (fourth), 1.00 (fifth), 0.81 (sixth), 0.70 (seventh), 0.58 (eighth), 0.48 (ninth), and -3.8 (reverse). The electrical drive system consists of a 400V three-phase brushless permanent magnet motor with a peak power of 160 kW and 660 n-m of peak torque with electrical power storage provided by a NiMH battery pack consisting of four liquid cooled 400V, 45 Ah NiMH batteries. The electric motor can also operate as generator with the ability to provide 75 kW of 3-Phase 50/60/400 Hz continuous export power. The output of the 9S70 and electric motor are combined and connected to a synchronised two-speed transfer case with a locking differential which drives identical front and rear axle differentials. Each axle uses an electronically controlled limited slip differential lock with planetary hub-reduction and hydraulic disc brakes with an integral anti-lock braking system (ABS). Front and rear winches with a capacity of up to 4,500 kilograms are also fitted to the vehicle as standard.

The Lynx uses double wishbone independent suspension with with 19 centimeters of suspension travel on both front and rear axles with ride height adjustable from between 37 to 51 centimeters. The vehicle is fitted with four wheel steering using a closed-loop feedback controller system with a wall to wall turning radius of 7.3 meters. The tires used in the vehicle are 365/80R20 tires with run-flat inserts. A central tire inflation system (CTIS) is fitted as standard having four predetermined terrain settings (Highway, Cross-Country, Mud & Snow, Emergency) and a Run Flat (RF) mode which checks tire pressures regularly and inflates tires as needed to compensate for leaks. The Lynx can achieve a maximum road speed of 130 km/h and is capable of overcoming 60% slopes, up to 40% of lateral tilt, and can cross 0.75 meter wide ditches and overcome vertical obstacles up to 0.5 meters in height. Fording depth is up to 1.5 meters without a snorkel.


Sensors & Electronics:
Panoramic Driver Vision Enhancer: For driving at night or in low-light level conditions the Lynx is fitted with a SDI Panoramic Driver Vision Enhancer (PDVE) module mounted above the cab which contains three 640 x 512 pixel 17 µm uncooled vanadium oxide (Vox) microbolometer sensors operating in the LWIR band (8-12µm) which combined provide a stitched 140° horizontal by 30° vertical field of view ahead of the vehicle. HDMI output from the panoramic DVE sensor is streamed at 30 Hz to an 800 x 600 pixel resolution driver’s vision enhancer (DVE) display & control module located on the vehicle dashboard which allows the driver to pan the entire 140° field of view with the DVE output scaled to the full display size.

Vehicle Multiband Networking Radio: For C4I and communications purposes the Lynx is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.

Integrated Driver Assist System: The Lynxcomes standard fitted with SDI's Integrated Driver Assist System (IDAS) system which includes forward collision warning (FCW), emergency brake assist (EBA), adaptive cruise control (ACC), lane departure warning (LDW), electronic stability control (ESC), and blind spot monitoring functions.

Forward collision warning (FCW) and emergency brake assist (EBA): The forward collision warning (FCW) and emergency brake assist (EBA) system employs a front facing 77 GHz millimeter wave (MMW) radar in the front bumper which is intended to detect moving and stationary vehicles or pedestrians in the vehicle's path. The system will then generate both audible and visual warnings and if necessary will automatically brake and de-throttle the engine if the driver does not react in time. Should the driver apply the brakes with insufficient force a dynamic brake support (DBS) system will increase the brake force above what the driver has applied in order to avoid a collision.

Adaptive cruise control (ACC): The adaptive cruise control (ACC) system employs the forward facing 77 GHz MMW radar along with a 24 GHz ground speed radar mounted with a 35° look down behind the forward wheel well and automatically adjusts the vehicle speed to maintain a safe distance from vehicles ahead on the road. The adaptive cruise control system is controlled by a lever attached to the steering column. Gently tapping the lever either up or down engages the adaptive cruise control and increases the cruise speed by one kilometer per hour. Pushing or depressing the lever further increases or decreases speed by five kilometres per hour. A knob on the lever is used to adjust following distance in one meter increments which is displayed on the central screen in front of the driver. Pushing the lever forward, braking, or accelerating will disable the adaptive cruise control.

Lane departure warning (LDW): The lane departure warning (LDW) system employs two sets of CCD cameras on either side of the crew cab which track the lane markings on either side of the vehicle and provide both an audible and visual warning to the driver when one of the lane markings is crossed without the turn signal being applied.

Electronic stability control (ESC): The electronic stability control (ESC) system is designed to mitigate severe oversteer or understeer conditions leading to vehicle loss of-control (LOC) as well as mitigating on-road rollovers by using a lateral acceleration sensor, yaw rate sensor, and steering wheel angle sensor to monitor the vehicle’s directional control and selectively applying the brakes at each wheel position and reducing engine power in order to help the driver regain control of the vehicle. The ESC will also maintain heading control by determining the driver’s intended heading via the speed and steering wheel angle sensors and automatically adjusting the steering behavior of the vehicle if the steering response does not match the driver’s intention.

Blind spot monitoring: The blind spot monitoring system employs two side looking 24 GHz short-range radars mounted either side of the crew cab with a 160° field of view which will generate a visual warnings for the driver when the radars detect the presence of cars or pedestrians located in one of the vehicle's blind spots. The system will generate an additional audible warning if the driver activates the turn signal while the system has detected an object in one of the vehicle's blind sports and will increase the resistance in the steering wheel if a driver attempts to change lanes while the system has detected an obstacle in one of the blind spots.

Autonomous Navigation System: In addition to the Integrated Driver Assist System the Lynx is fitted with SDI's autonomous navigation system (ANS) which permits fully autonomous on and off-road self-driving along with robotic convoy operations. The autonomous navigation system (ANS) includes terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. For detecting terrain and obstacles in front of the vehicle the ANS employs twin laser imaging perception modules (LIPMs) which each contain a 2-D scanning LADAR (LAser Detection And Ranging) sensor and two pairs of stereo color and infrared cameras. The LADAR sensors operate with a 905 nm wavelength at 75 Hz with 0.25°angular resolution and generate a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. Each LADAR sensor is augmented by a set of stereo camera pairs which use twin 1024 x 768 pixel CCD cameras and twin 320 x 240 pixel uncooled LWIR (8-12 μm) cameras with 90° FOV lenses which provide stereo range acquisition of terrain obstacles ahead of the vehicle and when combined with the LADAR sensors provides 3D imagery of terrain in the direction of travel.

The LADAR and stereo camera sensors along with ten wheel encoders, ten vehicle height management sensors HMS, a ground speed radar, and a forward looking 77 GHz millimeter wave (MMW) radar are coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer and a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation.

The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.

The autonomous navigation system of the vehicle can follow two different modes; autonomous mode and vehicle leader-follower mode. In autonomous mode the user selects one or more GPS waypoints using the control display which the vehicle will then drive to while autonomously detecting and avoiding any obstacles along the route. In vehicle leader-follower or “robotic convoy" mode the vehicle can be instructed to follow either a manned vehicle or another unmanned robotic convoy vehicle which it will attempt to follow at a specified distance using it's forward imaging perception sensors. Should the follower vehicle lose track of the 'leader' vehicle the follower will revert to GPS navigation using GPS waypoints received by the leader vehicle.


Variants:
Lynx Utility Vehicle: The Lynx utility is the base version and has a 2 person cab with a cargo bed that can hold 3,000 kilograms of payload and has an onboard crane capable of lifting 360 kilograms at a distance up to 2.4 metes. The utility vehicle can also be used to tow a 2-wheeled trailer with the same wheels and suspension as the Lynx which can carry an additional 2,500 kg of payload.

Lynx Ambulance: The ambulance variant of the Lynx adds an armored rear cab area with an NBC environment capable environmental control system with a gas particulate filter unit (GPFU) which can transport medical equitation and can hold up any combination of four patients on litters and eight seated patients.

Lynx Command and Control Vehicle: The command version of the Lynx is designed to act as a mobile command post and adds an armored rear cab area which contains a 10 kW lightweight APU, NBC environment capable environmental control system with a gas particulate filter unit (GPFU), two computer workstations, fiber optic local area network connections, and equipment racks for various command, control and communications equipment.
Last edited by The Technocratic Syndicalists on Tue Nov 16, 2021 4:47 pm, edited 16 times in total.
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Postby The Technocratic Syndicalists » Mon Nov 02, 2020 6:53 pm

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KfZ 310 Kodiak

General Characteristics:
  • Type: All-terrain amphibious vehicle
  • Weight: 15.5 t
  • Length: 8.0 m
  • Width: 2.45 m
  • Height: 2.0 m
  • Crew: 1 driver + 3 passengers (front cab), 8 passengers (rear cab)

Mobility:
  • Engine: AMG HL72 turbocharged inline 6-cylinder diesel, 240 kW (325 PS)
  • Transmission: AMG 6S130 (6 forward, 1 reverse gears)
  • Suspension: Torsion bar w/ adaptive dampening
  • Max road speed: 70 km/h
  • Max reverse speed: 10 km/h
  • Max water speed: 5 km/h
  • Fuel capacity: 320 l
  • Operational range: 500 km

Armament (optional):
  • 1x 8 mm MG 45E (1,000 rounds)

Maneuverability:
  • Power/weight Ratio: 20.9 PS/t (15.4 kW/t)
  • Ground pressure: 25 kPa
  • Ground clearance: 0.50 m
  • Gradient: 100%
  • Sideslope: 45%
  • Fording Depth: 1.5 m
  • Trench crossing: 2.0 m
  • Vertical wall climb: 1.1 m



Overview:
The Kettenfahrzeug 310 (Kfz 310) Kodiak is a tracked, articulated twin-cab amphibious vehicle designed by SDI Vehicle Systems. The Kodiak features an articulated steering system and an extremely low ground pressure and is designed to transport troops and equipment across deep snow, boglands, and other terrain impassible to other conventional wheeled or tracked vehicles.


Armament:
Scanfire RWS: The self-defense purposes the roof of the vehicle can be optionally fitted with an SDI Scanfire remotely operated weapon station. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers..


Protection:
Armor protection:The cabins of the Kodiak feature a monocoque construction made from welded >600 Brinell hardness ultra high hardness steel (UHHS) plates with internal M5 fiber/epoxy composite spall panels which provides each cabin with 360º protection against 7.62 mm armor piercing ammunition at a distance of 30 meters and 155 mm high explosive shell fragments at 60 meters. When used as an APC the vehicle can also be fitted with add-on bar/slat armor providing protection against RPGs and other shaped charge munitions. Although the vehicles ground pressure is low enough to avoid triggering the majority of anti-tank mines both cabins feature a V-shape bottom with steel deflector plates and a kevlar floor lining designed to protect against up to 6.0 kg TNT equivalent charge anti-tank mines detonating under the vehicle/

Fire extinguishing system: The crew, fuel, and powertrain compartments of the Kodiak include an automatic fire suppression system (AFES) which is designed to automatically extinguish fires that develop inside the vehicle. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the crew compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to both vehicle cabins and maintains cabin compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Mobility:
  • Name: HL72
  • Type: Multi-fuel diesel engine
  • Length: 1,090 mm
  • Width: 670 mm
  • Height: 920 mm
  • Dry Weight: 555 kg
  • Bore/stroke: 106/134 mm
  • Displacement, cylinder: 1.2 l
  • Displacement, total: 7.6 l
  • Compression ratio: 18:1
  • Charging method: Twin-scroll turbocharger
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 6 in-line
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 240 kW (325 PS) @ 2,200 RPM
  • Torque: 1300 N-m @ 1,400 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Kodiak is powered by an AMG HL72 6-cylinder in-line diesel engine producing 240 kW (325 PS) of power. The HL72 is a modified heavy duty truck engine and is a 7.2 liter displacement 6-cylinder water cooled disese; engine with a twin-scroll turbocharger air induction system with an air-water aftercooler. The HL72 engine is coupled to an AMG 6S130 automatic transmission with 6 forward and 1 reverse gears. The 6S130 has a 7.1:1 overall gear ratio spread with gear ratios being 4.59 (first), 2.25 (second), 1.54 (third), 1.00 (fourth), 0.75 (fifth), 0.65 (sixth), and -5.00 (reverse). The engine and transmission are mounted in the front cabin and the transmission output is connected through a 2-speed transfer gearbox (1.28 and 2.11 high and low gear ratios) to the differentials and final drives on both the front and rear cab drive sprockets through a propeller shaft running between the front and rear cabins. Hydraulic disk brakes are fitted to both differentials with a manual disk brake on the front differential as an emergency brake. The steering system does not use differential track speed and instead uses a hydraulically actuated pivot between the front and rear cabins which articulates the vehicle based on driver steering commands, preventing the possibility of differential track speeds causing the vehicle to slip on loose ground. The articulated steering system also makes the vehicle highly maneuverable with a turning circle diameter of 11 meters when fully loaded.

The Kodiak uses a semi-active hydraulic suspension system with 7 road wheels on the side of each cab. The suspension uses torsion bars springs and adaptive hydraulic dampeners on each road wheel arm to provide a smooth ride across the rough terrain the vehicle is designed to operate on. The vehicle uses 62 centimeter wide nylon reinforced rubber tracks resulting in a fully loaded ground pressure of only 25 kPa, a ground pressure less than half that of a walking person which allows the vehicle to traverse across snow, mud, and sand without sinking. The Kodiak is capable of climbing a 45 degree slope (100% gradeability) with a maximum side slope angle of 35 degrees and is capable of traversing gaps up to 2 meters wide and climbing over obstacles up to meter in height. The vehicle is also fully amphibious and using its tracks for propulsion can swim through the water at speeds up to 5 kilometers per hour.


Variants:
Troop carrier: Standard APC version which can carry up to 12 fully equipped troops or up to 5,500 kg of payload. Armament is an SDI RWS-100 with an MG 45E 8x57mm general purpose machine gun with 1,000 rounds mounted to the roof of the front cab. with the option to mount an additional MG 45E on a ring mount above the roof hatch on the rear cabin.

Logistics carrier: Cargo variant which replaces the rear cab with a flatbed load handling system which can carry a 3.0 meter length container or up to 8,000 kg of payload. The front cabin as well as vehicle handling and amphibious capability are identical to the base troop carrier version. Crew is a driver and co-driver who sit in the front cabin. Optional armament is an SDI RWS-100 with an MG 45E 8x57mm general purpose machine gun with 1,000 rounds mounted to the roof of the front cab.

Ambulance: Medical evacuation and treatment variant which can accommodate up to four stretchers or eight seated casualties in its rear cab. Carries a crew of five along with stretchers and various and medical equipment. Also carries a tent which folds out from the rear cab which can be used as a treatment area up to eight patients.

Command post:Modified APC variant equipped with long range radios and which carries a crew of up to six command staff in the rear cab and a driver plus up to three personnel in the front cab. The rear cab is modified to carry VHF/UHF multi channel radios and mounts an extendable 20 meter radio mast along with spare barriers and a 3 kVA diesel generator.

Mortar carrier: Mortar carrier which replaces the rear cabin of the APC version with a special shock-absorbing flatbed with armored sides and rear and open top which can mount either an 81mm mortar with up to 140 rounds or a 120mm mortar with up to 100 rounds. Crew is a driver and commander in the front cabin and a gunner and up to two loaders in the rear flatbed. Optional armament is an SDI RWS-100 with an MG 45E 8x57mm general purpose machine gun with 1,000 rounds mounted to the roof of the front cab.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:11 pm, edited 15 times in total.
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Postby The Technocratic Syndicalists » Fri Dec 11, 2020 10:12 am

Image

RKpz 401 Stalker

General Characteristics:
  • Type: Unmanned Ground Combat Vehicle (UGCV)
  • Weight: 3.2 t
  • Length: 3.5 m
  • Width: 2.1 m
  • Height: 2.4 m
  • Crew: 0

Mobility:
  • Engine: AMG HL20 multi-fuel 4-cylinder turbo diesel engine, 105 kW (140 PS)
  • Transmission: Diesel-electric drive, 4x 25 kW hub motors
  • Suspension: Walking beam
  • Max onroad speed: 80 km/h
  • Max offroad speed: 50 km/h
  • Operational range: 200 km

Armament:
  • 1x 40 mm GMG40, 70 rounds
  • 2x twin-tube ATGM launchers

Maneuverability:
  • Power/weight Ratio: [i]43.8 PS/t (32.8 kW/t)
  • Ground clearance: 0.35 m
  • Gradient: 60%
  • Sideslope: 40%
  • Fording depth: 1.0 m
  • Trench crossing: 1.0 m
  • Vertical wall climb: 0.50 m


Overview:
The Robotkampfpanzer 401 (RKpz 401) Stalker is an unmanned ground combat vehicle (UGCV) designed by SDI Vehicle systems. The Stalker features both integrated anti-tank and anti-personnel armament combined with autonomous navigation and reconnaissance, surveillance, and target acquisition (RSTA) sensors and can be controlled from an operator control station located in a manned ground vehicle or from a dedicated hand-held controller unit. Designed to be attached to light infantry units at the platoon and company level the Stalker can be operated either semi-autonomously or under remote control and is designed to support both infantry operations with direct machine gun and anti-armor weapons fire, provide over-watching surveillance and fire support, provide forward reconnaissance capability, and act as a mobile communications relay.


Armament:
The Stalker carries a remote turret which contains both a SDI GMG 40 40 mm grenade machine gun and four SSM-94 hypervelocity anti-tank guided missiles. The SDI GMG 40 is short-recoil operated, belt fed automatic grenade launcher capable of firing high velocity 40mm programmable air-burst grenades out to an effective range of 1,500 meters and is fed from a belt containing 70 40 x 53 mm rounds contained in a magazine inside the remote turret which can be reloaded using a hatch on the turret roof. The turret is actively stabilized and can rotated a full 360° at a rate of 60°/s while the GMG 40 can be elevated from -10° to +60° at a rate of 60°/s.


Protection:
The Stalker features a hull and turret constructed from 19 mm thick welded 2519-T87 aluminum-copper alloy plates which gives the vehicle all-around protection against 7.62 mm AP rounds at 30 meters and 155 mm artillery shell fragments at 60 meters. The vehicle's underbelly protection consists of a 19 mm thick 2519-T87 alloy belly plate which is designed to protect against 0.6 kg TNT equivalent blast mines.


Mobility:
  • Name: HL20
  • Type: Multi-fuel diesel engine
  • Length: 810 mm
  • Width: 780 mm
  • Height: 640 mm
  • Dry Weight: 135 kg
  • Bore/stroke: 83/92 mm
  • Displacement, cylinder: 0.5l
  • Displacement, total: 2.0 l
  • Compression ratio: 18:1
  • Charging method: Twin-scroll turbocharger
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 4 in-line
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 240 g/kW-hr
  • Power: 105 kW (140 PS) @ 4,200 RPM
  • Torque: 300 N-m @ 1,600 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Stalker is powered by an AMG HL20 inline four-cylinder turbo diesel engine rated at 140 PS (105 kW). The HL20 is used to drive a 100 kW liquid-cooled 3-phase permanent magnet synchronous generator which supplies 400VDC electrical power to four wheel hub motors, one for each track. Each hub motor is rated at 25 kW of maximum power and consists of a liquid cooled permanent magnet synchronous motor and multi-stage planetary gear reduction system contained inside the wheel hub. Thermal loads for both the diesel engine and hub motors are managed by a thermal management system with three water/glycol cooling loops; one for the engine, for the generator and hub motors, and a third for the engine charge air cooler. The vehicle's drivetrain has a total of eight wheels paired into four groups of two wheels with each pair of wheel covered by a rubber band track in a "track-over-wheel" arrangement with the outboard wheel in each track group being driven by a hub motor. The vehicle uses a semi-active walking-beam suspension with magnetorheological shock absorbers which can be used to control the vehicle ride height. The Stalker uses a skid-steering system to turn with the ability to turn in place, enhancing the vehicles maneuverability when navigating confined spaces or when traversing rough terrain.

The vehicle's electrical system employs twin 24VDC power busses; one for vehicle starting and drivetrain operation and the other for the vehicle's mission systems. Each power bus is connected to a separate engine driven alternator and is connected to its own rechargeable lithium-ion battery. Power from the second bus is further split by a power supply into 5, 12, and 24VDC power to supply the vehicle's various sensor, navigation, communication, and weapon systems. The vehicle also includes a 3.5 kW solid oxide fuel cell (SOFC) auxiliary power unit (APU) which uses the vehicle's diesel fuel supply. The APU can be switched on and off by the vehicle operator to give the vehicle a silent watch capability with the ability to operate the vehicle's surveillance sensors, weapons, and communications systems without main engine power.


Sensors & Control:
FLIR Sensor:The vehicle's FLIR sensor consists of a mast-mounted sensor turret which contains infrared, low-light, and visible imagers and laser rangefinder/designator/pointer mounted atop an extensible mast mounted to the vehicle's turret which provides day/night and all-weather sensing and target acquisition capability for detecting, classifying, and reporting hostile forces. The FLIR sensor turret contains a thermal imager with a 640 x 512 pixel InSb focal plane array (FPA) operating in the MWIR (3-5 μm) region with 40° to 21°field-of-view (FOV) and up to 4x digital zoom, a 3-Chip Color CCD-TV camera with a 1920 x 1080 pixel CCD sensor with 54.4° to 1.5° field-of-view (FOV) and up to 3x digital zoom, a low light level television (LLLTV) camera with a 1280 x 720 pixel sCMOS sensor with 52.1° to 1.4° field-of-view (FOV) and up to 3x digital zoom, a 10 kilometer range 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder, 1.06 μm Nd:YAG, laser designator, and 150 mW laser pointer. The sensor turret features 4-axis gimbal stabilization and can traverse a full 360°with -60° to +60° elevation capability. The sensor turret is mounted to a five-section extensible mast can be extended to a height of 3.0 meters above the turret roof. The FLIR sensor features far target location (FTL) capability which combine attitude and position information from two sight mounted differential GPS (DGPS) antennas and range data from the laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The RSTA sensor also automatic target recognition (ATR) capability using an imaging sensor autoprocessor (ISA) unit built into the sensor. The ISA employs parallel very high speed integrated circuit (VHSIC) processors contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, helicopters, and other vehicles. Targets identified by the sight can then be designated and engaged through networked fires from artillery, missiles, aviation, or using the vehicle's own weapons.

Autonomous navigation system: The Stalker's autonomous navigation system (ANS) comprises the vehicle's terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. The ANS also provides vehicle navigational state data for use by other vehicle systems external to the ANS including the vehicles weapons and surveillance sensors. For detecting terrain the ANS employs a steerable imaging perception module (IPM) mounted on top of the turret which contains a 180º scanning single-axis LADAR and and a passive stereo imaging system with three pairs of stereo cameras. The LADAR sensor operates with a 905 nm wavelength at 75 Hz with 0.25° angular resolution and generates a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. The LADAR sensor is augmented by three stereo camera pairs which uses twin 1024 x 768 pixel CCD cameras with 90° FOV lenses, twin 640 x 480 pixel low light level television (LLLTV) CMOS cameras, and twin 320 x 240 pixel uncooled LWIR (8-12 μm) cameras separated by a 24 centimeter baseline which provide stereo range acquisition of terrain obstacles and when combined with the LADAR sensors provides color 3D imagery of terrain in the direction of travel under day and night and low visibility conditions. The imaging perception module is coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer. The imaging perception and core navigation modules are coupled to a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation. The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.

Operator Control Station: The Stalker is controlled via an operator control station (OCS) located inside a manned armored vehicle which consists of a driving display, control display, and video game console style handheld controller. The driving display is a color LCS display which shows sensor feed from the Stalker vehicle's ANS system including camera feed from the vehicle's imaging perception modules and vehicle orientation and position data from the Stalker vehicle's INS/GPS system. In teleoperation mode video feed from the vehicle's cameras is streamed at a rate of 1-10 Mbps and is displayed in the center of the driving display. Data from the terrain perception algorithm is also overlaid onto the camera feed in order to warn the operator of any terrain obstacles in the vehicle's current path. Below the camera feed are four dials which display the vehicle's current speed, azimuth, pitch, and roll. As a way to prevent the operator from inadvertently flipping the vehicle the pitch and roll dials will flash red if the vehicle's pitch or roll exceeds 30°.The top right of the driver's display is used to display an overhead digital terrain elevation map of the area around the vehicle. The driving display will also alert the operator if the Stalker vehicle's fault detection system detects a fault in the vehicle through a flashing warning at the bottom of the display. Placed below the driving display is the control display, a touschscreen display used to control the vehicle's various operational modes and functions. In autonomous navigation mode the touschscreen display is used to plan routes using digital terrain maps of the area and to generate the GPS waypoints that the vehicle will follow when navigating autonomously. The control display also acts as a vehicle health monitoring display and will display the the location, type, and consequences of detected faults in addition to the warning message that appears in the driving display. The handheld controller is modified from a commercial video game console controller and is used for both driving and sensor and weapon control under teleoperation mode. When driving the vehicle the right joystick is used to steer the vehicle while the left joystick is used to control the vehicle speed. When driving one or both triggers (L1 or L2) must be continuously depressed, ensuring that the vehicle will come to a stop if the operator drops or looses control of the controller. When operating the turret or FLIR sensor the left joystick is used to control traverse, the right joystick used to control elevation, and the triggers used to control camera zoom. The Stalker vehicle to be controlled from the operator control console in four different modes; teleoperation mode, autonomous mode, vehicle leader-follower, and dismount leader-follower mode. In teleoperation mode the imagery and navigation data from vehicle's cameras and INS/GPS are streamed to a operator workstation in near-real time and the Stalker is steered remotely by the user using the hand held controller. In teleoperation mode a wireless LAN radio 2.4 GHz omni-directional datalink antenna with a UDP-based data transfer protocol is used to exchange data between the control station and vehicle which limits data transfer rate to 10 kbps for steering and control commands, 60 kbps for telemetry and 10 Mbps for video feed. An additional emergency stop radio (ESR) independent of the wireless LAN radio is also included in the communications system which acts as an indecent 'kill switch" to triggers system shutdown in both teleoperation and autonomous operation modes. In teleoperation mode should the vehicle loose radio contact with the control station it will enter a 'standby' mode, remaining still until control can be re-established. In autonomous mode the user selects one or more GPS waypoints using the control display which the vehicle will then drive to while autonomously detecting and avoiding any obstacles along the route. In vehicle leader-follower or “robotic convoy" mode the Stalker can be instructed to follow either a manned vehicle or another Stalker which it will attempt to follow at a specified distance using it's forward imaging perception sensors. Should the Stalker lose track of the 'leader' vehicle the Stalker will revert to GPS navigation using GPS waypoints received by the leader vehicle. Dismount leader-follower is identical to vehicle leader-follower except the Stalker is instructed to follow a walking person rather than a vehicle.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:12 pm, edited 31 times in total.
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OOC: Call me Techno for Short
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The Technocratic Syndicalists
Minister
 
Posts: 2173
Founded: May 27, 2015
Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Mon Dec 14, 2020 6:25 pm

Image

MiRpz 401

General Characteristics:
  • Type: Unmanned mine detection vehicle
  • Weight: 3.2 t
  • Length: 3.5 m
  • Width: 2.1 m
  • Height: 1.9 m
  • Crew: 0

Mobility:
  • Engine: AMG HL20 multi-fuel 4-cylinder turbo diesel engine, 105 kW (140 PS)
  • Transmission: Diesel-electric drive, 4x 25 kW hub motors
  • Suspension: Walking beam
  • Max onroad speed: 80 km/h
  • Max offroad speed: 50 km/h
  • Operational range: 200 km

Maneuverability:
  • Power/weight Ratio: 43.8 PS/t (32.8 kW/t)
  • Ground clearance: 0.35 m
  • Gradient: 60%
  • Sideslope: 40%
  • Fording depth: 1.0 m
  • Trench crossing: 1.0 m
  • Vertical wall climb: 0.50 m
Last edited by The Technocratic Syndicalists on Wed Nov 03, 2021 4:23 pm, edited 5 times in total.
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Postby The Technocratic Syndicalists » Mon Dec 14, 2020 6:28 pm

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RTpz 401

General Characteristics:
  • Type: Unmanned equipment transport vehicle
  • Weight: 3.8 t
  • Length: 3.5 m
  • Width: 2.1 m
  • Height: 1.9 m
  • Crew: 0

Mobility:
  • Engine: AMG HL20 multi-fuel 4-cylinder turbo diesel engine, 105 kW (140 PS)
  • Transmission: Diesel-electric drive, 4x 25 kW hub motors
  • Suspension: Walking beam
  • Max onroad speed: 80 km/h
  • Max offroad speed: 50 km/h
  • Operational range: 200 km

Maneuverability:
  • Power/weight Ratio: 36.8 PS/t (27.6 kW/t)
  • Ground clearance: 0.35 m
  • Gradient: 60%
  • Sideslope: 40%
  • Fording depth: 1.0 m
  • Trench crossing: 1.0 m
  • Vertical wall climb: 0.50 m


Overview:
The RTpz 401 is an amphibious unmanned ground vehicle (UGV) designed by SDI Vehicle systems. The Tpz 401 shares the same chassis as SDI's RKpz 401 unmanned ground combat vehicle (UGCV) and replaces the turret of the RKpz 401 with a cargo bed which can accommodate up to 1,400 kg of payload and it intended to act a robotic cargo vehicle with the ability to carry three squads worth of equipment and supplies and follow both vehicles and dismounted infantry over a variety of terrain conditions.


Mobility:
  • Name: HL20
  • Type: Multi-fuel diesel engine
  • Length: 810 mm
  • Width: 780 mm
  • Height: 640 mm
  • Dry Weight: 135 kg
  • Bore/stroke: 83/92 mm
  • Displacement, cylinder: 0.5l
  • Displacement, total: 2.0 l
  • Compression ratio: 18:1
  • Charging method: Twin-scroll turbocharger
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 4 in-line
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 240 g/kW-hr
  • Power: 105 kW (140 PS) @ 4,200 RPM
  • Torque: 300 N-m @ 1,600 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Sensors & Control:
Autonomous navigation system: The vehicle's autonomous navigation system (ANS) comprises the vehicle's terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. The ANS also provides vehicle navigational state data for use by other vehicle systems external to the ANS including the vehicles weapons and surveillance sensors. For detecting terrain the ANS employs a steerable imaging perception module (IPM) mounted on top of the hull which contains a 180º scanning single-axis LADAR and and a passive stereo imaging system with three pairs of stereo cameras. The LADAR sensor operates with a 905 nm wavelength at 75 Hz with 0.25° angular resolution and generates a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. The LADAR sensor is augmented by three stereo camera pairs which uses twin 1024 x 768 pixel CCD cameras with 90° FOV lenses, twin 640 x 480 pixel low light level television (LLLTV) CMOS cameras, and twin 320 x 240 pixel uncooled LWIR (8-12 μm) cameras separated by a 24 centimeter baseline which provide stereo range acquisition of terrain obstacles and when combined with the LADAR sensors provides color 3D imagery of terrain in the direction of travel under day and night and low visibility conditions. The imaging perception module is coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer. The imaging perception and core navigation modules are coupled to a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation. The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.
Last edited by The Technocratic Syndicalists on Tue Nov 16, 2021 4:48 pm, edited 7 times in total.
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Postby The Technocratic Syndicalists » Thu Dec 17, 2020 6:55 pm

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TrFz 303

General Characteristics:
  • Type: Artillery reconnaissance vehicle
  • Weight: 27.0 t
  • Length: 6.8 m
  • Width: 3.4 m
  • Height: 2.0 m
  • Crew: 3 (driver, commander, radar operator)

Mobility:
  • Engine: 2x AMG HL44 multi-fuel twin-turbo V4 diesel engines, 400 kW (550 PS) each
  • Transmission: Diesel-electric; 2x 300 kW traction motors, 2x 150 kW steering motors
  • Suspension: Active in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 950 l (200 Gallons)
  • Operational range: 750 km

Armament:
  • 1x 8 mm MG-45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 37.0 PS/t (27.4 kW/t)
  • Ground clearance: 0.50 m
  • Ground pressure: 0.70 kg/cm2
  • Gradient: 60%
  • Sideslope: 30%
  • Fording depth: 1.5 m
  • Trench crossing: 2.6 m
  • Vertical wall climb: 1.1 m


Overview
The Trägerfahrzeug 303 (TrFz 303) is an armored, tracked, radar reconnaissance and surveillance vehicle which is designed to provide day, night, all weather target moving target detection, artillery fire observation, and weapon locating capability in support of friendly artillery unit. The TrFz 303 uses the same chassis as SDI Vehicle System's PzKfz 303 armored personnel carrier which has been modified with the addition of a extending mast containing radar and FLIR sensors along with the addition of external fuel tanks (EFTs), artillery plotting equipment, and additional long-range radio communications systems.


Protection:
Armor Protection: The hull of the vehicle is constructed from friction stir welded (FSW) 2139-T8 aluminum alloy plates 40 mm thick which provides the hull 360° protection against 15mm AP ammunition at 200 meters and 155 mm high explosive shell fragments at 30 meters. The base armor is augmented by ceramic armor panels containing tandem silicon-carbide (SiC) tiles embedded into a cast 7075 alloy aluminum matrix which along with the base armor provide frontal arc protection (+/- 30°) against 30 mm APFSDS rounds at 500 meters and 360° protection against 155 mm high explosive shell fragments at 10 meters. The inside surface of the vehicle features a borated spall liner consisting of orthogonally cross-plied M5 ballistic fibers laminated into a flexible borated polyethylene resin which serves to minimize the post-armor effect of penetrating projectiles and shaped charge jets and to provide radiation protection for the crew and electronics inside the vehicle. Under-belly protection is provided by an armored V-hull which provides protection against EFP and 10kg TNT equivalent blast anti-tank mines. Additionally the four vehicle crew members located in the hull sit on blast-attenuating seats with no direct contact to the vehicle floor

Fire extinguishing system: The crew, ammunition, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFSS) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire. When a fire is detected inside the vehicle Halon 1301 contained in several pressurized bottles each with fast-reacting solenoid-actuated valves is sprayed into the compartment to extinguish the fire. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Propulsion
  • Name: HL44
  • Type: Multi-fuel diesel engine
  • Length: 890 mm
  • Width: 450 mm
  • Height: 740 mm
  • Dry Weight: 450 kg
  • Bore/stroke: 115/105 mm
  • Displacement, cylinder: 1.1 l
  • Displacement, total: 4.4l
  • Charging method: two-stage variable-geometry turbocharger
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 4, inline
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 400 kW @ 4,300 RPM
  • Torque: 910 N-m @ 3,800 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Sensors:
FMG 200 Battlefield Surveillance Radar: The vehicle is equipped with an SDI FMG 200 X-band (8-10 GHz) pulse-doppler active electronically scanned array (AESA) radar system mounted to a six-section extendable mast which allows the radar system to be raised to a height of 6.8 meters above the vehicle roof in less than 60 seconds from its stowed position. The radar and mast are stored in a armored, waterproof box-shaped enclosure on top of the vehicle which the radar system retracts into when not in use. The radar itself employs a phased array antenna 0.6 meters wide and 0.7 meters tall using air-cooled GaN (Gallium-nitride) T/R modules and can be steered electronically +/- 60° and mechanically tilted +/- 20° in elevation along with the ability to be rotated mechanically a full 360°. The radar transmits with up to 7 watts of power and has a maximum instrumented range of 40 kilometers with the capability of detecting small UAVs at 7 kilometers, walking personnel at 15 kilometers, light aircraft at 22 kilometers, trucks and other large vehicles at 30 kilometers, and low-flying helicopter at 30 kilometers with the ability to track up to 500 simultaneous targets. In artillery spotting and counter-battery mode the radar is capable of detecting fired 105 mm artillery shells at 12 kilometers and fired 155 mm artillery shells at 18 kilometers with a weapon locating accuracy of +/- 10 meters in range and +/- 2 meters in azimuth. The radar interface includes a fiber optic LAN (Local Area Network) for radar control which is used to transmit data output of plots, tracks and equipment status to the radar control station inside the vehicle along with an additional LAN interface used for optical camera control.

Optical observation system: In addition to the radar the vehicle also includes an optical observation and reconnaissance system which is mounted to the masr above the radar antenna and boresighted to the radar antenna line-of-sight. The optical observation system consists of a box shaped housing which measures 36.0 by 53.0 by 43.5 centimeters and contains a 1280×720 pixel infrared camera with an Indium Antimonide (InSb) detector operating in the MWIR (3 - 5 μm) region with two selectable fields of view including 24°x13.5° WFOV (Wide Field of View) and 1.9°x 1.08° NFOV (Narrow Field of View) with 12x optical and 16x digital zoom capability, a CCD color camera with 1920 x 1080 pixel resolution and two selectable fields of view including 63°x 35° WFOV (Wide Field of View) and 2.3°x1.3° NFOV (Narrow Field of View) with 30x optical and 12x digital zoom capability, a 10 kilometer range 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder with <1 meter range accuracy, and an 860 nm laser pointer/illuminator. The sensor can be elevated from -30° to +70° and like the radar can be rotated a full 360° in azimuth. The optical observation sensor features far target location (FTL) capability which combines attitude and position information from two sight mounted differential GPS (DGPS) antennas and range data from the laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 20 kilometers.


Situational Awareness:
Driver Vision Enhancer: The vehicle features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 12 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the vehicle while under hatch. The STAS system consists of four camera modules placed at the corners of the hull which each contain two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions. Each STAS module also contains an imaging sensor autoprocessor (ISA) similar to the one in the gunner and commander FLIR sights which provides automatic target recognition (ATR) capability of threats detected by the system. The STAS can be used to monitor the area around the vehicle during silent watch or while the crew is asleep and includes automatic alert broadcast and target-tracking/moving-target indicator functions which can track detected threats and can interface with the fire control system to hand-off threats to the gunner or commander's sight for immediate engagement by the tank's main or coaxial armament.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:13 pm, edited 11 times in total.
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Postby The Technocratic Syndicalists » Mon Dec 28, 2020 12:28 pm

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Brlpz 151 Mammoth

General Characteristics:
  • Type: Armored vehicle-launched bridge
  • Weight: 63.5 t
  • Length: 15.0 m
  • Width: 4.0 m
  • Height: 3.95 m
  • Crew: 2 (driver, bridge operator)

Mobility:
  • Engine: AMG HL280 multi-fuel quad-turbo V12 diesel engine, 1,765 kw (2,400 PS)
  • Auxiliary power unit: SDI RKM700 turbocharged rotary engine, 60 kW (80 PS)
  • Transmission: AMG AK 7-700 hydrokinetic transmission (7 forward, 3 reverse gears)
  • Suspension: Active in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 65 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 1,300 l
  • Operational range: 550 km

Bridge System:
  • Gap crossing length: 24.0 m (26.0 meter bridge length)
  • Bridge load capacity: >90 t
  • Crossing speed: 13-16 kph
  • Launch time: <5 min
  • Recovery Time: 10 min

Maneuverability:
  • Power/weight Ratio: 34.6 PS/t (25.2 kW/t)
  • Ground clearance: 0.55 m
  • Ground pressure: 0.95 kg/cm2
  • Gradient: 70% m
  • Sideslope: 40%
  • Fording Depth: 1.4 m
  • Trench Crossing: 3.0 m
  • Vertical Wall Climb: 1.3 m


Overview
Brückenlegepanzer 151 (Brlpz 151) Mammoth is an armored bridge-laying variant of the PzKpfw 151 Tiger main battle tank designed by SDI Vehicle Systems. The vehicle consists of a modified PzKpfw 151 Tiger chassis fitted with bridge-laying gear and a cantilever type assault bridge instead of a turret and is designed to support combat gap crossing capability with the same off-road mobility, survivability, and transportability as the PzKpfw 151


Bridging Equipment:
Heavy Assault Bridge: The Brlpz 151 is equipped with an SDI Vehicle Systems Heavy Assault Bridge (HAB), a horizontally deployed cantilever type assault bridge which consists of four interchangeable steel and aluminum alloy sections which create a 26 meter long bridge for crossing gaps up to 24 meters across. The complete 26 meter long bridge is 4.0 meters wide, weighs 10.9 tonnes, and is designed to support crossing of MLC 90+ tracked and MLC 100+ wheeled vehicles at speeds up to 16 km/h. Using a trestle two 26 meter bridges from two Brlpz 151 vehicles can also be combined end-to-end to allow gaps of up to 48 meters to be crossed. Unlike scissor-type assault bridges the Heavy Assault Bridge is deployed horizontally which avoids raising the vehicle's silhouette during bridge laying operations. The bridge can be deployed in 4 minutes and can be retrieved from either end in around ten minutes. The hydraulics for the bridge deployment mechanism are powered by the vehicle's APU and allow the bridge to be deployed and recovered without the vehicle's engine running. The bridge launch and recovery can be accomplished by a single crew member using a set of bridging controls and a graphical display which is fitted to both the driver and commander compartments of the vehicle. The front of the vehicle is also equipped with a dozer blade attached to the lower glacis which can be used to anchor the vehicle for bridge laying operations and to clear out obstacles to prepare the bridging site.


Protection:
Armor Protection:The Brlpz 151 Mammoth has the same heavy-metal composite armor system as fitted to the PzKpfw 151 main battle tank which is designed to provide protection against kinetic energy (KE) threats in the form of long-rod penetrators fired by high-pressure tank cannons and chemical energy (CE) threats including large-caliber shaped charge munitions. The composite armor covers the front and sides of the the hull with the remainder of the vehicle protected only by conventional steel armor. The armor is designed to provide frontal /- 30° protection against large caliber tank gun fired APFSDS rounds (800-1000 mm RHA penetration) and large caliber anti-tank guided missiles (~170mm diameter SC with 1500-1600 mm RHA penetration) and 360° protection against 15mm AP ammunition and handheld anti-tank weapons (110mm diameter SC). Appropriate average RHA equivalent protection for the glacis across the frontal 60 degree arc is 1,000-1,200 mm RHA against kinetic-energy munitions and 1,800-2,200 mm versus chemical-energy munitions. In the addition to the composite armor the inside of the hull is fitted with spall panels to minimize the post-armor effects of rounds which penetrate into the vehicle.

Fire extinguishing system: The crew, fuel, and powertrain compartments of the vehicle include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the diver's compartment which through a series of hoses and pipes spray Halon agent into the fighting compartment or ammunition engine compartment when the system detects a fire. The system can also be manually activated through a panel in the driver's compartment. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Mobility:
  • Name: HL280
  • Type: Multi-fuel diesel engine
  • Length: 1,750 mm
  • Width: 780 mm
  • Height: 950 mm
  • Dry Weight: 1,890 kg
  • Bore/stroke: 150/135 mm
  • Displacement, cylinder: 2.30 l
  • Displacement, total: 27.6 l
  • Charging method: Quad variable-geometry sequential turbochargers
  • Intercooling: Air-oil intercooler and aftercooler
  • Number of Cylinders: 12, V, 60 degrees
  • Cooling method: Oil cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 1,765 kW (2,400 PS) @ 3,300 RPM
  • Torque: 6,890 N-m (5080 ft-ib) @ 2,000 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Situational Awareness:
Driver Vision Enhancer:The vehicle features both front and rear mounted driver vision enhancer (DVE) sensor units which provide both front and rear facing thermal and low-light-level color television imagery to assist the driver when driving the vehicle at night or in adverse weather conditions. Each DVE sensor consists of an 640 x 480 pixel uncooled long-wave infrared (8 - 12 μm) detector and a low-light level (400 - 1000 nm) CCD camera with fixed 1x magnification and a 55° x 40° field of view. The DVE features sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying of weather, light, and road conditions.

See-Through Armor System: The vehicle is equipped with an SDI See-Through Armor System or STAS which provides 360 degree panoramic view of the surroundings around the vehicle while under hatch. The STAS system consists of four camera modules mounted to the corners of the hull each containing two 640 × 480 pixel long-wave infrared (8-12 µm) thermal imagers with a 58° by 45° FOV each and two ultra-high resolution color CMOS daylight CCD cameras with a 95° by 78° FOV which are set at a 90° angle from each other. Each STAS module measures 200 x 100 x 250 mm and weighs 10 kilograms and features a ballistic protection cover to protect the cameras from shrapnel and small arms fire. The STAS system with four sensor modules provide overlapping 360 °field-of-view day and night vision around the tank and is capable of detecting a person sized target out to 800 meters (900 meters with the daylight channel) and like the DVE units feature sensor fusion of the IR and CCD camera output which is selectable from 0% IR/100% visible to 100% IR /0% visible to allow for optimum visibility in a varying weather and light conditions.


Communications & Remote Control:
Vehicle Multiband Networking Radio: The primary radio system of the vehicle is an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the rear of the vehicle's hull. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable inter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.


Battle Management:
SDI Arcturus Battle Management System (ABMS): Arcturus is a wireless tactical network system designed by SDI which provides blue force tracking, command and control (C2), communications network management, and decision-making support at the brigade/regiment level and below. The complete Arcturus Battle Management System (ABMS) vehicle installation consists of a blue force tracker (BFT) transceiver, central processor unit, commander's display unit, keyboard unit, a removable hard disk drive cartridge (RHDDC), and an interface to the vehicle's software defined radio which is used to transmit friendly and enemy locations, battlefield situational awareness reports, operational maps, and command and control (C2) messages in real time to other Arcturus equipped platforms. The commander's display unit is a 30.5 centimeter 1024x768 pixel XGA touch-screen display connected to a 3.1 GHz processor unit with up to 16 GB DDR3 RAM and a 512GB solid state hard drive and provides an electronic map with digital terrain elevation data (DTED) information, an own vehicle position/orientation indicator which displays the vehicle's current GPS grid position and orientation on the map in real time, and various situational awareness overlays including the locations of other platforms (friendly in blue, enemy in red) along with other tactical symbiology which is overlaid onto the map display. An 85-key QWERTY keyboard is attached to the display and is environmentally sealed to protect against dirt, dust and moisture and includes a sealed mouse pointer and USB port for data input. The blue force tracking hardware consists of a ground vehicle transceiver contained on a single line replaceable unit (LRU) measuring 20 x 20 x 15 cm and weighing 2.75 kg which contains an omnidirectional phased array SATCOM antenna which provides two-way X band (7.9-8.4 GHz transmit and 7.25-7.75 GHz receive) full-duplex satellite communications with AES 256-bit bulk encryption at uplink and downlink rate of up to 131 kb/s with 5° to +90° elevation and 360° azimuth coverage around the vehicle. Blue force tracking information includes the unit's current GPS grid position and heading as measured by its INS/GPS system as well as fuel, ammunition, communication, and vehicle health status which is transmitted as a track file to other Arcturus equipped units every five minutes or after the vehicle has traveled a distance of 800 meters. Using the same SATCOM system the vehicle commander can also use the keyboard attached to his commander's display unit (CDU) to communicate with other units on the Arcturus network with various types of text message up to 500 characters long, lowering the radio traffic of equipped units. The system can also transmit various pre-programmed text messages which can be sent with a single button press. Message types supported by the system include enemy destroyed/damaged, friendly destroyed/damaged, NBC alerts, fragmentary orders (FRAGORDs), minefield alerts, call for indirect fire, call for CAS, contact reports, weather reports, route reports, engagement updates, ammo status/request, fuel status/request, position status/update, shell/bomb/missile/mortar damage reports, and requests or status for other reports. The commander can also use the touchscreen display to draw and transmit graphic overlays on the digital terrain map indicating enemy positions, terrain features or obstacles, fire support plan overlays, or other information which is then overlaid onto the digital maps of all units on the network.


AI Modules:
To aid in the performance of the crew the vehicle includes a series of artificial intelligence (AI) modules run on the vehicle's central processor including navigation aids, situational report and assessment, and C3 (command, control, and communications).

Navigation Aiding Module: the navigation aiding module is a driving and mission planning aid which combines own vehicle position information from the vehicle's INS/GPS system, terrain data from three-dimensional digital terrain elevation data (DTED) maps of the current terrain stored in the Arcturus central processor, and data received from the Arcturus network including the type, status, position, and heading of friendly forces, and intelligence reports received over the Arcturus network including the location, status, and activity of enemy units. The data is fused by the navigation module and superimposed on the commander's display unit indicating the location and display of friendly and enemy units. Data displayed on the commander's display includes the unit type (ie tank, APC, helicopter), unit position (GPS grid location and elevation), unit heading (degrees), unit status (moving, stopped, engaged, destroyed), and data time stamp (day/hour/minute). Using this information the navigation module calculates and displays viewsheds for enemy and friendly weapons as a function of sensor type, time of day, terrain, and ambient weather conditions and highlights danger zones on the map display where friendly units will be in the viewshed of enemy sensors and weapons. For movement operations the route planning capability of the navigation aid can then generate on-road and off-road routes to navigate to a user specified navigation point that minimizes both travel time, elevation change, and exposure to enemy sensors and weapons. The best navigation routes along with estimates with confidence intervals on travel distance and enemy exposure are displayed to the commander who can then choose which route he wished to follow. After the vehicle commander selects a desired route the route information is transmitted to the driver's display and to other vehicles in the commander's unit. During movement the system then prompts the driver with directions to follow and will continuously update it's route planning calculation with new information and prompt the commander if the system detects a new alternate route with less exposure and/or travel time than the currently selected ones. The navigation module also also includes a deployment planning capability to determine ideal vehicle positions for defensive or overwatch operations. Using the mouse, keyboard, and touchscreen on his commander's display the commander can select an area on the map he wants his unit to cover where the module will then determine the terrain positions which provide the best weapon and sensor viewsheds over the selected terrain.

Situational Report & Assessment: The situational report & assessment (SR&A) module is an analyzer module which processes current and past intelligence reports received over the Arcturus network and makes guesses about future enemy actions and activity. The SR&A does not directly interface with any sensors and instead collects, analyses and then displays intelligence data on the commander's display module. Data the SR&A analyses includes track files on friendly and enemy vehicle which includes the vehicle type (APC, tank, helicopter, etc), grid position and elevation, heading, IFF status (friendly, enemy, or unknown), damage status (operational, damaged, destroyed), sensor used to detect (ie FLIR, radar, visual) and derived data (LOS range, weapon viewshed) along with current terrain and weather data (light and visibility conditions, rain/snow/wind/fog, etc) and intelligence data in the form of estimated enemy ORBATs and tactics. The SR&A takes this data and then makes interference about future enemy behavior using a pre-programmed rule set with various scenarios modeling potential enemy behavior. Output from the SR&A module includes visual warnings on the commander's display alerting him to expected enemy actions or when the system detects a major change in its current situation assessment as well as the system's generated intelligence reports which are stored on the processor system's hard drive.

Command, Control, and Communications (C3): The Command, Control, and Communications or C3 module is responsible for centralized control of all vehicle external communications systems including UHF/VHF line-of-sight radio and SATCOM communications and controls the generation, transmission, and reception of communications messages. The C3 module also maintains a list of every node in the vehicle's current network with their current status and time of last transmitted or received message. Communications messages include track files from the blue force tracking systems, text messages, and IFF transmissions. The C3 module also attempts to maintain low probability of intercept (LPI) by reducing transmission frequency when in proximity of enemy forces and adaptively reducing communication power to the minimum needed to reach the recipient.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:14 pm, edited 7 times in total.
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Postby The Technocratic Syndicalists » Mon Dec 28, 2020 12:30 pm

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PzKfz 303 Marten

General Characteristics:
  • Type: Armored personnel carrier
  • Weight: 30.0 - 35.0t (depending on variant)
  • Length: 6.8 m
  • Width: 3.4 m
  • Height: 2.0 m
  • Crew: 3 (driver, gunner, commander) + 8 dismounts

Mobility:
  • Engine: 2x AMG HL44 multi-fuel twin-turbo V4 diesel engines, 400 kW (550 PS) each
  • Transmission: Diesel-electric; 2x 300 kW traction motors, 2x 150 kW steering motors
  • Suspension: Active in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 950 l
  • Operational range: 750 km

Armament:
  • 1x 8 mm MG-45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 37.0 PS/t (26.7 kW/t)
  • Ground clearance: 0.50 m
  • Ground pressure: 0.70 kg/cm2
  • Gradient: 60%
  • Sideslope: 40%
  • Fording depth: 1.5 m
  • Trench crossing: 2.6 m
  • Vertical wall climb: 1.0 m


Overview
The Panzerkettenfahrzeug 303 (PzKfz 303) Marten is a modular armored fighting vehicle designed by SDI vehicle systems. The PzKfz 303 is designed as an armor personnel carrier with a chassis which can be readily converted to reconnaissance, ambulance, control vehicle, or other turreted variants.


Armament
Scanfire RWS: The base APC version of the Marten is fitted with an SDI Scanfire remotely operated weapon station. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers.

Smoke-grenade launchers: The base APC version of the vehicle is equipped with a total 16 smoke grenade launchers grouped into two sets of 4-tube launchers on either side of the vehicle's roof which cover the forward two 90º sectors. The smoke launchers fire 66mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The launchers are controlled manually from a panel in the commander's station which can fire individual grenades or salvos of four across each forward 90 degree sector.


Protection:
Armor Protection: The hull of the vehicle is constructed from friction stir welded (FSW) 2139-T8 aluminum alloy plates 40 mm thick which provides the hull 360° protection against 14.5 mm AP ammunition at 200 meters and 155 mm high explosive shell fragments at 30 meters. The base armor can be augmented by ceramic armor panels containing tandem silicon-carbide (SiC) tiles embedded into a cast 7075 alloy aluminum matrix which along with the base armor provide frontal arc protection (+/- 30°) against 30 mm APFSDS rounds at 500 meters and 360° protection against 152 and 155 mm high explosive shell fragments at 10 meters. The inside surface of the vehicle features a borated spall liner consisting of orthogonally cross-plied M5 ballistic fibers laminated into a flexible borated polyethylene resin which serves to minimize the post-armor effect of penetrating projectiles and shaped charge jets and to provide radiation protection for the crew and electronics inside the vehicle. Under-belly protection is provided by an armored V-hull which provides protection against EFPs and 10kg TNT equivalent blast anti-tank mines. Additionally the four vehicle crew members located in the hull sit on blast-attenuating seats with no direct contact to the vehicle floor.

Fire extinguishing system: The crew, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFSS) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire. When a fire is detected inside the vehicle Halon 1301 contained in several pressurized bottles each with fast-reacting solenoid-actuated valves is sprayed into the compartment to extinguish the fire. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Propulsion
  • Name: HL44
  • Type: Multi-fuel diesel engine
  • Length: 890 mm
  • Width: 450 mm
  • Height: 740 mm
  • Dry Weight: 450 kg
  • Bore/stroke: 115/105 mm
  • Displacement, cylinder: 1.1 l
  • Displacement, total: 4.4l
  • Charging method: two-stage variable-geometry turbocharger
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 4, inline
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 400 kW @ 4,300 RPM
  • Torque: 920 N-m @ 3,800 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Marten uses a diesel-electric drive system consisting of twin diesel engines and integrated starer/generator units places in the hull sponsons and a mechanically regenerated hybrid electro-mechanical cross-drive transmission located in the front of the hull which combines the power input of the traction and steering motors and distributes it to the twin drive sprockets. The mechanical decoupling of the diesel engines with the drive sprockets allows for the engines to run at a constant RPM, improving fuel efficiency, while the use of two diesel propulsion units and twin steering and traction motors in the transmission provides a high level of redundancy and resistance to damage. The packaging of the diesel engines in the hull sponsons also serve to increase the effective internal volume of the hull for crew, weapons, and other payload.

Engine: The engine used in each powerpack is an AMG (Arkaenisch Motorenfabrik Gesellschaft) HL44, a four cylinder inline, common rail fuel fuel injection, twin sequentially charged low-heat rejection diesel engine which outputs a maximum 400 kW of power at 4,300 rpm. The engine also includes an integral oil-cooled permanent magnet synchronous flywheel starter-generator unit which is geared to the engine output shaft using a speed-increasing transfer case with a fixed 4.2:1 gear ratio. The HL44 employs a common rail fuel-injection system with a fuel rail running the length of the engine and twin hydraulic boost pumps running at up to 3,100 rpm to pressurize the fuel to 1,800 bar for injection into each cylinder. Turbocharging is accomplished with twin single-stage variable-geometry turbocharger units using variable-area turbine nozzles which providing boost pressure ratios up to 5:1. A water-to-air charge-air cooler is placed after the turbocharger compressor stages to cool and density the air before entering the combustion chambers. To maximize engine performance across a broad ambient temperature spectrum the water and oil cooling system of the engine are split into a high temperature loop which cools the piston liners, cylinder heads, and other engine components along with the first stage of the charge-air cooler, and a low temperature loop which cools the power electronics, engine oil, and the second stage of the charge-air cooler. A dual-circuit water pump circulates cooling water through both the high and low temperature loops and then through the radiator cooling system which employs twin 30 kilowatt variable-speed fans to cool the coolant before it's passed into the expansion tank and then circulated again through the twin coolant loops. An integrated flywheel starter generator is used to start the engine and is rated for mechanical input power of up to 400 kW and outputs 3 phase 60 Hz 600 VAC alternating current The starter-generator is a self-excited, brushless, oil cooled, permanent magnet machine using neodymium-iron-boron permanent magnets and has a rated speed of 18,000 RPM, necessitating a 4.2:1 gear ratio speed-increaser gearbox be placed between the generator and engine. Other engine accessories including inlet air filter system, turbo intercooler and aftercooler circuits, charge air cooler with inlet manifold, exhaust scrubber and infrared suppression system, and oil filter and cooler, are included in the power pack as a single engine unit. The left and right hand side powerpacks are identical and can be fitted to either side of the vehicle. The powerpack additionally includes the oil cooling system with air-oil heat exchanger and a hydrostatically driven cooling fan.

Transmission: The vehicle powertrain system employs a mechanically regenerated cross-drive transmission which reduces the required motor power required to drive and regeneratively brake each drive sprocket. The transmission system includes twin 150 kilowatt oil-cooled permanent magnet synchronous steering motors and twin 300 kilowatt oil-cooled permanent magnet synchronous traction motors located on either sides of the transmission. Both traction and steering motors employ a rotor with samarium-cobalt magnets and a ferromagnetic core with an inconel superalloy sleeve and have a maximum rated speed of 18,500 RPM with a 93% efficiency at a base speed of 4,600 RPM. The steering and traction motors on either side of the transmission are supplied electrical power through a generator converter box located in each sponson ahead of the the powerpack which converts the three phase 600 volt AC power from the engine generators into 600 volt DC power which is transferred to a DC bus located on either side of the cross drive unit which then supplies DC power to the motor inverters and the various accessory drives. The cross drive unit itself contains a central drive shaft connected to a differential gearbox which combines the inputs from the two steering motors and two traction motors to power the drive sprockets through the planetary reduction final drive assemblies located on either side of the cross-drive transmission. A two speed oil-cooled planetary reduction gearbox with twin hydraulically actuated clutches is additionally incorporated into the cross-drive transmission and connects the central differential to the steering and traction motors to reduce the required rpm and torque ranges of the electrical steering and traction motors. The cross drive additionally contains an oil cooled wet disk brake and a parking brake unit.

Suspension & Running Gear: The suspension system used by the vehicle is an SDI designed semi-active in-arm hydro-pneumatic suspension system with three sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (12 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The vehicle's running gear features a decoupled design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle's road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units. Instead of conventional steel tracks the vehicle employs composite rubber band tracks which are 50% lighter and result in a 70% vibration reduction and 10 dB noise reduction inside the vehicle at a road speed of 50 kph. The tracks are 550 mm wide with a 120 mm pitch and have a designed durability of over 5,000 km before needing replacing.


Variants:
The PzKfz 303 is made in three basic versions including a basic platform, a raised roof platform and a heavy weapon platform. The basic platform includes the PzKfz 303 APC, BPzA 303 forward observer vehicle, and TrFz 303 radar carrier vehicle variants. The raised roof version features a larger and higher rear compartment with increased internal volume for the crew and other equipment and includes the PzBfw 303 command and communications vehicle, FltPzA 303 artillery fire direction control vehicle, FltPzM 303 mortar fire direction vehicle, and SKfz 303 armored ambulance. The heavy weapon platform version features a reinforced chassis with a turret wing to enable the fitting of heavy weapons and includes the PzM 303 self propelled mortar variant.

PzKfz 303: Base armored personnel carrier variant. Carries a crew of 3 with 8 passengers and armed with an SDI Scanfire remote weapon station carrying a machine gun or automatic grenade launcher.

BPzA 303: Artillery forward observer vehicle variant of the PzKfz 303. The vehicle carries a crew of three and is equipped with a 2 meter mast equipped with a long range thermal camera, CCD camera, laser range finder, and differential GPS receiver. Armament consists of an SDI Scanfire remote weapon station carrying a machine gun or automatic grenade launcher.

TrFz 303: Radar reconnaissance variant of the variant of the PzKfz 303 equipped with an SDI FMG 200 battlefield surveillance radar along with an electro-optical targeting system mounted atop an extending 6 meter mast. Armament consists of an SDI Scanfire remote weapon station carrying a machine gun or automatic grenade launcher.
Last edited by The Technocratic Syndicalists on Sun Jan 16, 2022 7:36 pm, edited 15 times in total.
SDI AG
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International Freedom Coalition


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IC: The Kingdom of Arcaenia

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The Technocratic Syndicalists
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Posts: 2173
Founded: May 27, 2015
Inoffensive Centrist Democracy

Postby The Technocratic Syndicalists » Mon Dec 28, 2020 12:40 pm

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sFH 78GW Marksman

General Characteristics:
  • Type: Self Propelled Howitzer
  • Weight: 48,000 kg
  • Length: 11.3 m
  • Width: 2.4 m
  • Height: 3.9 m
  • Crew: 2

Mobility:
  • Engine: AMG HL80 multi-fuel twin-turbo V8 diesel engine, 740 kW (1,000 PS)
  • Transmission: Diesel-electric transmission; 735 kW AC generator, 10x 100 PS -Induction motors
  • Suspension: Hydropneumatic
  • Brakes: Disc brakes with ABS (Anti-Lock Braking System)
  • Tires: 10 (+1) 16R20 with run-flats and CTIS (Central Tire Inflation system)
  • Steering: 5-axle with power assist
  • Max road speed: 105 km/h
  • Fuel capacity: 950 l
  • Operational range: 1,000 km
  • Ground clearance: 0.60 m

Armament:
  • 1x 17 cm artillery gun, 30 rounds
  • 1x 8 mm MG 45E, 1000 rounds

Maneuverability:
  • Gradient: 70%
  • Side slope: 40%
  • Fording Depth: 1.5 m
  • Trench Crossing: 2.5 m
  • Vertical Wall Climb: 0.6 m


Overview
The Marksman is a wheeled self-propelled howitzer designed by SDI Vehicle Systems. The Marksman system consists of an SDI HTTS 10x10 chassis which is mated to an artillery gun module containing a 17 cm L/60 howitzer and a fully automated ammunition and propellant charge loading system contained in a remote turret at the rear of the vehicle. The complete Marksman Artillery System consists of a single howitzer vehicle and an ammunition resupply vehicle which employs the same SDI HTTS chassis as the howitzer vehicle.


Armament
SDI 17 cm L/60 sFK 78 Howitzer:
  • Barrel Length: 60 calibers
  • Projectiles: SDI 17 cm series
  • Charges: SDI AM95 modular unicharge system, Zones 1-7
  • Muzzle Velocity: 1,115 m/s (AM95 zone 7)
  • Chamber Pressure: 430 MPa (AM95 zone 7)
  • Range Hollow Base (HB): 48 km (AM95 zone 7)
  • Range Base Bleed (BB): 65 km (AM95 zone 7)
  • Range Base-Bleed/Rocket-Assist (BB/RA): 85 km (AM95 zone 7)
The vehicle's main armament is The 17 cm L/60 sFH 78 Howitzer, a 17 cm howitzer with a 60 caliber length barrel. The barrel is of autofrettage monoblock construction with the gun barrel and breach plated with an explosively bonded tantalum alloy refractory liner for increased barrel life. The end of the barrel also includes a slotted muzzle brake to reduce recoil force. The recoil system is a conventional hydropneumatic recuperator mechanism with two recoil cylinders, internal hydraulic replenisher, recoil buffer and two recuperator cylinders. The breech mechanism is a multi-lug horizontally sliding breech block with an integral pulsed neodymium: ytterbium aluminum garnet (Nd:YAG) laser ignition system for ignition of the propellant charges. After firing some of the EGW mixture is sprayed into the chamber to extinguish residual propellant embers, clean the laser window, wet the breech seal and further cool the propellant chamber to prevent ammunition cook-off.

The cannon is designed to fire all SDI 17 cm ammunition and uses SDI's AM95 Bi-Modular Charge System (BMCS), a seven-zone modular charge system consisting of low and high zone combustible-case charges containing a polymer bonded RDX based insensitive propellant. With a full seven high zone propellant charges the muzzle velocity with a 66.8 kilogram projectile is 1,115 m/s and maximum range up to 48 kilometers with boat tailed/hollow base ammunition, 65 kilometers with base bleed ammunition, and up 85 kilometers using rocket assisted/base bleed projectile. The cannon with modular charge system and fire-control system supports Multiple Round Simultaneous Impact (MRSI) with 8 round simultaneous impact capability at ranges up to 40 kilometers (with base-bleed ammunition) with less than 4 second time between first and last round impact. Traverse of the turret and elevation of the cannon is achieved through brushless DC servomotors with a traverse range of +/-85° and elevation range of -1° to +70° with <0.3 milliradian pointing accuracy in both elevation and azimuth.

The cannon features an autoloader mechanism with projectile and propellant loading of the cannon being fully automated and requiring no human intervention. The projectile magazine can hold 21 fuzed projectiles while the propellant magazine holds 126 AM95 propellant charge modules. The maximum rate of fire is 3 rounds in 15 seconds or 21 rounds in 3 minutes with a maximum continuous rate of fire of 1.5 rounds per minute.

Secondary armament: For protection against close in threats the vehicle is fitted with an SDI Scanfire remotely operated weapon station mounted to the cabin roof which includes an MG 45E machine gun and electro-optical sensor suite. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. The weapon station includes dual-axis gyro-stabilization to allow for effective fire while the vehicle is moving. The weapon station is traversed and elevated using brushless DC servomotors and features -15 to +70 degrees elevation and 360 degrees of traverse. The sensor system includes a CCD daylight camera with up to 10x magnification, an uncooled 640 x 480 pixel LWIR (long wave infrared) imager, and an eye-safe Nd:YAG laser rangefinder. An ammunition box containing 1,000 rounds of 8x57 mm ammunition is stored ready for use on the weapon station.


Protection:
Armor protection: The HTTS chassis used by the Marksman vehicle features a fully armored cab constructed from welded 5 mm 600 BHN hardness ultra-high-hardness steel (UHHS) plates with integral silicon carbide (SiC) ceramic/polyethylene (UHMWPE) composite armor panels, ballistic glass windows, and an inner M5 fiber/epoxy composite spall liner which provides 360º azimuth and 0 - 30°elevation protection against 7.62 mm tungsten core armor piercing ammunition at a distance of 30 meters and 155 mm high explosive shell fragments at 60 meters. Under body protection for the crew cab consists of a multi-layered internal V-hull with a kevlar floor lining and mine blast protective crew seats which is designed to withstand a 10 kg TNT equivalent explosive blast AT Mine denoting under center or an 8 kg TNT equivalent explosive mass AT Mine detonating under one of the wheels.

Fire extinguishing system: The crew cab, fuel tanks, ammunition compartment, and powertrain compartments of the HTTS include an automatic fire extinguishing system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew cab are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the floor of the crew cab which through a series of hoses and pipes spray Halon agent into the crew or engine compartment when the system detects a fire. The system can also be manually activated through a panel near the driver's seat. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System:The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew cab and maintains cab pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing absorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously‘on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Mobility
  • Name: HL80
  • Type: Multi-fuel diesel engine
  • Length: 1,080 mm
  • Width: 700 mm
  • Height: 760 mm
  • Dry Weight: 830 kg
  • Bore/stroke: 109/107 mm
  • Displacement, cylinder: 1.00 l
  • Displacement, total: 8.00 l
  • Charging method: Twin variable-geometry turbochargers
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 8, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 210 g/kW-hr
  • Power: 735 kW (1,000 PS) @ 4,250 RPM
  • Torque: 2,050 N-m @ 2,750 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Sensors & Electronics:
Panoramic Driver Vision Enhancer: For driving at night or in low-light level conditions the cab of the HTTS chassis of the vehicle is fitted with a SDI Panoramic Driver Vision Enhancer (PDVE) module which contains three 640 x 512 pixel 17 µm uncooled vanadium oxide (Vox) microbolometer sensors operating in the LWIR band (8-12µm) which combined provide a stitched 140° horizontal by 30° vertical field of view ahead of the vehicle. HDMI output from the panoramic DVE sensor is streamed at 30 Hz to an 800 x 600 pixel resolution driver’s vision enhancer (DVE) display & control module located on the vehicle dashboard which allows the driver to pan the entire 140° field of view with the DVE output scaled to the full display size.

Vehicle Multiband Networking Radio: For C4I and communications purposes the vehicle is equipped with an SDI VHF/UHF Multiband Networking Radio (VMNR) which enables line-of-sight and beyond-line-Of-sight communication in the 30 MHz-2.5 GHz range. The VMDR is a four-channel, full-duplex, software defined radio which provides transmission of voice, video, and ISR data in the Narrowband VHF (30-225 MHz), UHF ( 225-520 MHz, 762-874 MHz), UHF SATCOM: (292-318 MHz transmit and 243-270 MHz receive). Wideband UHF (25-520 MHz), and L-band (762 MHz-2.5 GHz) communication bands. The complete VMNR system consists of a network information security unit, four universal transceivers, VHF and UHF power amplifiers, two wideband power amplifiers, and two omnidrectional VHF/UHF whip antennas mounted to the roof of the vehicle's unmanned turret. The SDI VMNR radio is designed to use a time-division multiple access (TDMA) networking waveform and like the Highband Tactical Radio is designed to enable unter-battalion and inter-brigade black core self-forming and self-healing mobile ad hoc network (MANET) operation with the ability to support up to 200 simulate nous nodes with transmit speeds up to 8 Mbbps.

Integrated Driver Assist System: The HTTS chassis used by the Marksman comes standard fitted with SDI's Integrated Driver Assist System (IDAS) system which includes forward collision warning (FCW), emergency brake assist (EBA), adaptive cruise control (ACC), lane departure warning (LDW), electronic stability control (ESC), and blind spot monitoring functions.

Forward collision warning (FCW) and emergency brake assist (EBA): The forward collision warning (FCW) and emergency brake assist (EBA) system employs a front facing 77 GHz millimeter wave (MMW) radar in the front bumper which is intended to detect moving and stationary vehicles or pedestrians in the vehicle's path. The system will then generate both audible and visual warnings and if necessary will automatically brake and de-throttle the engine if the driver does not react in time. Should the driver apply the brakes with insufficient force a dynamic brake support (DBS) system will increase the brake force above what the driver has applied in order to avoid a collision.

Adaptive cruise control (ACC): The adaptive cruise control (ACC) system employs the forward facing 77 GHz MMW radar along with a 24 GHz ground speed radar mounted with a 35° look down behind the forward wheel well and automatically adjusts the vehicle speed to maintain a safe distance from vehicles ahead on the road. The adaptive cruise control system is controlled by a lever attached to the steering column. Gently tapping the lever either up or down engages the adaptive cruise control and increases the cruise speed by one kilometer per hour. Pushing or depressing the lever further increases or decreases speed by five kilometers per hour. A knob on the lever is used to adjust following distance in one meter increments which is displayed on the central screen in front of the driver. Pushing the lever forward, braking, or accelerating will disable the adaptive cruise control.

Lane departure warning (LDW): The lane departure warning (LDW) system employs two sets of CCD cameras on either side of the crew cab which track the lane markings on either side of the vehicle and provide both an audible and visual warning to the driver when one of the lane markings is crossed without the turn signal being applied.

Electronic stability control (ESC): The electronic stability control (ESC) system is designed to mitigate severe oversteer or understeer conditions leading to vehicle loss of-control (LOC) as well as mitigating on-road rollovers by using a lateral acceleration sensor, yaw rate sensor, and steering wheel angle sensor to monitor the vehicle’s directional control and selectively applying the brakes at each wheel position and reducing engine power in order to help the driver regain control of the vehicle. The ESC will also maintain heading control by determining the driver’s intended heading via the speed and steering wheel angle sensors and automatically adjusting the steering behavior of the vehicle if the steering response does not match the driver’s intention.

Blind spot monitoring: The blind spot monitoring system employs two side looking 24 GHz short-range radars mounted either side of the crew cab with a 160° field of view which will generate a visual warnings for the driver when the radars detect the presence of cars or pedestrians located in one of the vehicle's blind spots. The system will generate an additional audible warning if the driver activates the turn signal while the system has detected an object in one of the vehicle's blind sports and will increase the resistance in the steering wheel if a driver attempts to change lanes while the system has detected an obstacle in one of the blind spots.
Last edited by The Technocratic Syndicalists on Sun Jun 19, 2022 7:18 pm, edited 13 times in total.
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Postby The Technocratic Syndicalists » Mon Dec 28, 2020 12:43 pm

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PzH 103

General Characteristics:
  • Type: Self Propelled Howitzer
  • Weight: 29.0 t
  • Length (hull): 7.9 m
  • Length (gun forward): 9.7 m
  • Width: 3.0 m
  • Height: 3.2 m (hull)
  • Crew: 3 (driver, gunner, commander)

Mobility:
  • Engine: AMG HL160 multi-fuel twin-turbo V8 diesel engine, 600 kW (820 PS)
  • Water drive: 2x shrouded propellers, 13.5 kN thrust each
  • Transmission: AMG 7S300 (7 forward, 1 reverse gears)
  • Suspension: Independent hydropneumatic
  • Max road speed: 105 km/h
  • Max water speed: 13.5 km/h
  • Fuel capacity: 560 l
  • Operational range: 1,000 km land, 70 km water

Armament:
  • 1x SDI LeFH 97 105mm L/52 howitzer, 56 rounds
  • 1x 8mm MG 45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 28.1 PS/t (20.7 kW/t)
  • Ground clearance: 0.45 m
  • Gradient: 70%
  • Sideslope: 40%
  • Trench crossing: 2.0 m
  • Vertical wall climb: 0.6 m
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 6:35 pm, edited 7 times in total.
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Postby The Technocratic Syndicalists » Tue Jan 26, 2021 7:24 pm

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RKpz 301 Hammerhead

General Characteristics:
  • Type: Unmanned Ground Combat Vehicle (UGCV)
  • Weight: 10.8 t
  • Length (hull): 5.0 m
  • Width: 2.4 m
  • Height: 2.0 m
  • Crew: 0 (1 remote)

Mobility:
  • Engine: AMG HL120 turbocharged V6 diesel, 230 kW (310 PS)
  • Transmission: AMG 6S160 hydromechanical transmission (6 forward, 3 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 70 km/h
  • Max offroad speed: 50 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 360 l
  • Operational range: 400 km

Armament:
  • 1x MK50 50 mm chain gun, 100 rounds
  • 1x 8 mm MG 45E, 1,000 rounds
  • 4x RBS 94 Lance Hypervelocity ATGMs

Maneuverability:
  • Power/weight Ratio: 28.7 PS/t (21.3 kW/t)
  • Ground clearance: 0.40 m
  • Gradient: 70%
  • Sideslope: 40%
  • Fording depth: 1.0 m
  • Trench crossing: 1.7 m
  • Vertical wall climb: 0.6 m


Overview:
The Hammerhead is an unmanned ground combat vehicle (UGCV) designed by SDI Vehicle systems. The Hammerhead features both integrated anti-tank and anti-personnel armament combined with target aquisition and autonomous navigation sensors and is designed to be controlled from an operator control station located in a manned ground vehicle. Designed to be attached to mechanized infantry units at the platoon and company level the Hammerhead can be operated either semi-autonomously or under remote control and is designed to support both vehicle and dismounted infantry operations with direct cannon, machine gun, and anti-tank missile fire, provide over-watching surveillance and fire support, provide forward reconnaissance capability, and act as a mobile communications relay.


Mobility:
  • Name: HL120
  • Type: Multi-fuel diesel engine
  • Length: 1,190 mm
  • Width: 1,020 mm
  • Height: 1,130 mm
  • Dry Weight: 940 kg
  • Bore/stroke: 130/150 mm
  • Displacement, cylinder: 2.0 l
  • Displacement, total: 12.0 l
  • Compression ratio: 18.5:1
  • Charging method: Twin-scroll turbocharger
  • Intercooling: Air-water intercooler and aftercooler
  • Number of Cylinders: 6 in-line
  • Cooling method: Water cooled
  • Injection method: Common rail injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 230 kW (310 PS) @ 1,800 RPM
  • Torque: 1550 N-m @ 1,100 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel


Sensors & Control:
Independent Thermal Sight: The vehicle's primary surveillance and targeting sensor is a two-axis stabilized independent thermal sight which is located on the turret roof. The main features of the sight are a third generation dual-wavelength (3-5 um and 8-14 um) thermal imager and high-resolution color CCD imager with 2-axis independently stabilized line of sight, ballistic computer, eye-safe laser rangefinder, and integrated GPS/inertial navigation system. The third generation thermal imager used with the gunner's sight is a 1280 x 1024 pixel dual color (MWIR and LWIR) capable Mercury cadmium telluride (HgCdTe) staring focal plane array (FPA) detector based system which features an architecture common to several other SDI designed third gen thermal imaging systems. The thermal imager is cooled using a Stirling cycle linear drive cryocooler which cools the detector assembly to 77°K. The detector and crycooler system are contained in a single Standard Advanced Dewar Assembly (SADA), a closed-cycle dewar-cooler assembly containing the linear crycooler, infrared FPA, Dewar, and various control electronics and sensors. The dual-color thermal imager features a color fusion system which assigns colors to pixel values from each MWIR and LWIR band (red for LWIR, cyan for MWIR), adding color contrast to the otherwise black-and-white thermal image. The thermal sight can be toggled between 3x magnification wide field of view (WFOV), 10x magnification medium field of view (MFOV), x25 narrow field-of view (NFOV), and x50 ultra-narrow field of view settings. Mounted alongside the thermal imager is a 1920 x 1080 pixel visible/near IR monochrome CCD camera with selectable 10x NFOV and 3x MFOV optical magnification with additional x25 narrow and x50 ultra-narrow magnification digital zoom capability which provides the sight with an additional daylight channel in addition to the dual-band thermal channel. An image fusion function is also available combines the data from the dual-band thermal imager and the CCD camera to provide a fused image selectable on the sight control panel from 100% visible / 0% IR to 0% visible / 100% IR in infinitely variable increments. Range information for the fire-control system is provided by a 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder which provides range data accurate to 1 meter from ranges of 80 meters up to 20 kilometers. The sight additionally contains a 1064 nm laser designator, laser illuminator and laser spot tracker. The sight's dual axis stabilized head mirror assembly provides for enhanced on-the-move (OTM) stabilization capability, ensuring the reticle of the sight stays stabilized in the center of the sight while the vehicle is on the move. Dual-axis stabilization is provided by micromachined 2-axis hemispherical Resonator Gyroscopes (HRGs) with 0.001 °/hour drift capability integrated into the sights inertial measurement unit (IMU) system. The sight is further integrated with a GPS/INS navigation system which inputs accurate heading, attitude, velocity and position information of the vehicle into the sight's ballistic computer. The navigation system combines 3 axis fiber optic gyroscopes, 3 axis pendulous accelerometers, and digital magnetic compass with further sensor input from vehicle motion sensor (VMS) systems in the drivetrain and two lightweight, jam resistant DGPS antenna integrated into either side of the sight housing. Attitude information from the GPS is used to give the sight far target location (FTL) capability which combines data from the GPS/INS system and laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The sight also includes automatic target recognition (ATR) capability using an imaging sensor autoprocessor (ISA) unit built into the sensor. The ISA employs parallel very high speed integrated circuit (VHSIC) processors contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, helicopters, and other vehicles. Targets identified by the sight can then be designated and engaged through networked fires from artillery, missiles, aviation, or using the vehicle's own weapons.

Autonomous navigation system: The vehicle's autonomous navigation system (ANS) comprises the vehicle's terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. The ANS also provides vehicle navigational state data for use by other vehicle systems external to the ANS including the vehicles weapons and surveillance sensors. For detecting terrain the ANS employs four LADAR (LAser Detection And Ranging) sensors and four sets of stereo color cameras mounted to the front turret face. The LADAR sensors are mounted to inertially stabilized “nodding” platforms for a wider field of view and operate with a 905 nm wavelength at 75 Hz with 0.25° angular resolution and generate a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. The LADAR sensors are augmented by four sets of stereo camera pairs which uses twin 1024 x 768 pixel CCD cameras with 90° FOV lenses hich provide stereo range acquisition of terrain obstacles and when combined with the LADAR sensors provides color 3D imagery of terrain in the direction of travel. The turret also mounts wide and narrow field of view color driing cameras and an infrared driving camera for use in teleoperation mode. The LADAR and stereo camera sensors are coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer and a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation. The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.

Operator Control Station: The Hammerhead is controlled via an operator control station (OCS) located inside a manned armored vehicle which consists of three large multifunction touchscreen displays with bezel buttons for display and crewstation controland a video game console style handheld controller used for remote vehicle control and target acquisition. Each multifunction touchscreen displays can be used to display two different information displays including the driving display, control display remote sensor feed, mission planning information, and digital terrain map displays. In teleoperation mode video feed from the vehicle's driving cameras is streamed at a rate of 1-10 Mbps and is displayed in the center multifunction display. Data from the terrain perception algorithm is also overlaid onto the camera feed in order to warn the operator of any terrain obstacles in the vehicle's current path. Below the camera feed are four dials which display the vehicle's current speed, azimuth, pitch, and roll. As a way to prevent the operator from inadvertently flipping the vehicle the pitch and roll dials will flash red if the vehicle's pitch or roll exceeds 30°. The top right of the driver's display is used to display an overhead digital terrain elevation map of the area around the vehicle. The display will also alert the operator if the vehicle's fault detection system detects a fault in the vehicle through a flashing warning at the bottom of the display. display is the control display, a touschscreen display used to control the vehicle's various operational modes and functions. In autonomous navigation mode the touschscreen display is used to plan routes using digital terrain maps of the area and to generate the GPS waypoints that the vehicle will follow when navigating autonomously. The display also acts as a vehicle health monitoring display and will display the the location, type, and consequences of detected faults in addition to the warning message that appears in the driving display.

The handheld controller is modified from a commercial video game console controller and is used for both driving and for sensor and weapon control under teleoperation mode. When driving the vehicle the right joystick is used to steer the vehicle while the left joystick is used to control the vehicle speed. When driving one or both triggers (L1 or L2) must be continuously depressed, ensuring that the vehicle will come to a stop if the operator drops or looses control of the controller. When operating the turret or FLIR sensor the left joystick is used to control traverse, the right joystick used to control elevation, and the triggers used to control camera zoom. The vehicle cam be controlled from the operator control console in four different modes; teleoperation mode, autonomous mode, vehicle leader-follower, and dismount leader-follower mode. In teleoperation mode the imagery and navigation data from vehicle's cameras and INS/GPS are streamed to a operator workstation in near-real time and the Stalker is steered remotely by the user using the hand held controller. In teleoperation mode a wireless LAN radio 2.4 GHz omni-directional datalink antenna with a UDP-based data transfer protocol is used to exchange data between the control station and vehicle which limits data transfer rate to 10 kbps for steering and control commands, 60 kbps for telemetry and 10 Mbps for video feed. An additional emergency stop radio (ESR) independent of the wireless LAN radio is also included in the communications system which acts as an indecent 'kill switch" to triggers system shutdown in both teleoperation and autonomous operation modes. In teleoperation mode should the vehicle loose radio contact with the control station it will enter a 'standby' mode, remaining still until control can be re-established. In autonomous mode the user selects one or more GPS waypoints using the control display which the vehicle will then drive to while autonomously detecting and avoiding any obstacles along the route. In vehicle leader-follower or “robotic convoy" mode the Stalker can be instructed to follow either a manned vehicle or another Stalker which it will attempt to follow at a specified distance using it's forward imaging perception sensors. Should the follower vehicle lose track of the 'leader' vehicle the follower will revert to GPS navigation using GPS waypoints received by the leader vehicle. Dismount leader-follower is identical to vehicle leader-follower except the vehicle is instructed to follow a walking person rather than a vehicle..
Last edited by The Technocratic Syndicalists on Wed Sep 15, 2021 2:22 pm, edited 16 times in total.
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Postby The Technocratic Syndicalists » Tue Mar 02, 2021 7:55 pm

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RbJPz 310

General Characteristics:
  • Type: Tank destroyer
  • Weight: 15.5 t
  • Length: 8.0 m
  • Width: 2.45 m
  • Height: 2.0 m
  • Crew: 2 (driver + gunner/commander)

Mobility:
  • Engine: AMG HL72 turbocharged inline 6-cylinder diesel, 240 kW (325 PS)
  • Transmission: AMG 6S130 (6 forward, 1 reverse gears)
  • Suspension: Torsion bar w/ adaptive dampening
  • Max road speed: 70 km/h
  • Max reverse speed: 10 km/h
  • Max water speed: 5 km/h
  • Fuel capacity: 320 l
  • Operational range: 500 km

Armament:

Maneuverability:
  • Power/weight Ratio: 20.9 PS/t (15.4 kW/t)
  • Ground pressure: 25 kPa
  • Ground clearance: 0.50 m
  • Gradient: 100%
  • Sideslope: 45%
  • Fording Depth: 1.5 m
  • Trench crossing: 2.0 m
  • Vertical wall climb: 1.1 m
Last edited by The Technocratic Syndicalists on Sat Feb 05, 2022 4:50 pm, edited 6 times in total.
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Postby The Technocratic Syndicalists » Tue Apr 20, 2021 5:50 pm

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RKpz 101 Wolverine

General Characteristics:
  • Type: Unmanned Ground Combat Vehicle (UGCV)
  • Weight: 24.5 t
  • Length (hull): 6.1 m
  • Length (gun forward): 10.5 m
  • Width: 2.6 m
  • Height: 2.4 m
  • Crew: 0 (1 remote)

Mobility:
  • Engine: AMG HL66 turbocharged V6 diesel, 550 kW (750 PS)
  • Transmission: AMG AK 6-200 hydrokinetic transmission (6 forward, 6 reverse gears)
  • Suspension: In-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 570 l
  • Operational range: 650 km

Armament:
  • 1x 105 mm L/73 smoothbore gun, 44 rounds
  • 1x 8 mm MG 45E, 1,000 rounds
  • 1x 40mm GMG 40, 48 rounds

Maneuverability:
  • Power/weight Ratio: 30.6 PS/t (22.5 kW/t)
  • Ground clearance: 0.41 m
  • Gradient: 70%
  • Sideslope: 40%
  • Fording depth: 1.0 m
  • Trench crossing: 2.1 m
  • Vertical wall climb: 0.8 m


Overview
The Wolverine is an unmanned ground combat vehicle (UGCV) designed by SDI Vehicle systems. The Wolverine is designed primarily to act as a robotic wingman for manned armored fighting vehicles and is designed to maneuvers in tandem with manned main battle tank and infantry fighting vehicles while providing direct-fire support with its high velocity smoothbore cannon. In addition to acting as a robotic wingman the Wolverine can be used to provide over-watching surveillance and fire support and act as an armed reconnaissance vehicle.


Armament:
Main gun:The primary armament of the Wolverine is an SDI 105mm L/73 smoothbore gun which is housed in an remote turret located in the center of the vehicle. The turret is fully stabilized and uses electric turret drives which can traverse the turret a full 360º at up to 40°/s and elevate from -10º to +20º at 40°/s with < 0.3 mrad pointing accuracy in both traverse and elevations. Originally designed as a main battle tank armament the 105mm L/73 gun weighs 1,950 kg and consists of a monobloc gun barrel 73 calibers long weighing 1,300 kg constructed from swage-autofrettaged electro-slag refined (ESR) steel with a 1,100 MPa yield strength which is attached to a vertical sliding wedge breech mechanism. Recoil reduction features added to the 105mm L/65 gun for use on the Wolverine include an integral pepperpot muzzle brake and a longer 760 mm recoil stroke which combined reduce the recoil by force by around half compared to the original weapon.

The gun fires fixed 105 mm ammunition including SDI AM346 APFSDS-T and AM344 HE-T rounds which are stored facing downwards in a electrically driven carousel style autoloader located underneath the turret in the turret basket. The autoloader can hold up to 44 rounds of ammunition in two concentric closed-loop rings of canisters. When the vehicle's operator selects an ammunition type (APFSDS-T or HE-T) the autoloader's magazine drive unit rotates the magazine so the closest APFSDS-T or HE-T round inside of its canister is aligned underneath the gun breech where the autoloader transfer unit then extracts the round, rotates it to align with the gun axis, and then rams it into the breech where the round can then be fired. After firing the spent casing is then extracted by the autoloader transfer mechanism and ejected through a door at the rear of the turret. By reversing the loading process the autoloader transfer mechanism unfired rounds in the gun can also be extracted and then returned to the autoloader carousel in the event of a cease-fire order or if the vehicle operator wishes to change the loaded munition type. The autoloader is capable of loading the gun at any elevation from -10º to +20º and allows for a sustained rate of fire of 12 rounds per minute. Reloading the autoloader is done using the case ejection port at the rear of the turret which allows the autoloader to be replenished in the field at a rate o 6 to 8 rounds per minute.

Secondary Armament: An 8mm MG 45E machine gun is mounted coaxial to the main armament with 1,000 rounds stored ready to fire in the turret. The turret of the vehicle additionally includes an SDI GMG 40 40mm grenade-machine gun (GMG) mounted to a remote weapon station attached to the vehicle's independent thermal sight (ITS) on top of the turret. The SDI GMG 40 is short-recoil operated, belt fed automatic grenade launcher capable of firing high velocity 40mm programmable air-burst grenades out to an effective range of 1,500 meters. The weapon station includes a box containing a 48 round belt ready to fire.

Smoke-grenade launchers: The vehicle is equipped with a total 16 smoke grenade launchers grouped into two sets of 4-tube launchers on either side of the turret face which cover the forward two 90º sectors. The smoke launchers fire 66mm diameter red phosphorus smoke grenades which provide effective obscuration across the entire visual and infrared (NIR, MWIR, LWIR) spectrum for countering TV, EO/IR, laser, and SACLOS guided weapons. The smoke grenade launchers are controlled automatically through an interface to the vehicle's laser warning sensors and launch smoke grenades automatically when the vehicle is illuminated by a hostile laser rangefinder or laser designator. The launchers can also be fired manually by the vehicle operator which can choose to fire individual grenades or salvos of four across each forward 90 degree sector.


Protection:
The Wolverine features a hull and turret constructed from friction stir-welded 2139-T8 aluminum alloy plates 25 mm thick augmented with 75mm thick bolted-on applique armor panels consisting of hexagonal hot-isostatic-presssed (HIP) silicon carbide (SiC) tiles embedded in a forged 7075 aluminum alloy matrix which provides the vehicle with frontal +/- 30° protection against 30 mm APFSDS at 500 meters, 360° protection against 14.5 mm AP rounds at 100 meters, and 360° protection against 155 mm shell fragments at 10 meters. The hull side protection of the vehicle is augmented by a total of 60 heavy explosive reactive armor (ERA) modules bolted to the vehicle's side skirts which provide additional protection against large diameter shaped charge and tank gun fired APFSDS ammunition. Each ERA module employs a metal-free composite construction and contains two reactive layers and a passive layer consisting of ceramic composite plates sandwiching an explosive or inert elastomer layer (respectively). The vehicle also features a layer of ceramic composite roof armor which provides top protection against artillery delivered shaped charge bomblets up to 70 mm in diameter. The inside of the vehicle is fitted with a spall liner consisting of multiple layers of orthogonally cross-plied M5 ballistic fibers laminated into a flexible thermoplastic resin. The spall liner serves to reduce the spall cone angle of spall fragments, reducing the spread of fragments inside the vehicle and minimizing the chances that a penetrating round will disable any of the vehicle's electrical or mechanical systems. Protection against mines is provided by a 25 mm thick 2139-T8 aluminum alloy belly plate and a layer of bolt-one ceramic belly armor which is designed to protect the vehicle against 6.0 kg TNT equivalent blast mines.

Fire extinguishing system: The ammunition and powertrain compartments of the Wolverine include an automatic fire suppression system (AFES) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the engine and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire which active the fire suppression system when compartment temperature exceed 80 degrees C. Four 9 kg pressurized bottles containing Halon 1301 fire suppressing agent are located in the hull which through a series of hoses and pipes spray Halon agent into the ammunition or engine compartments when the system detects a fire. The system can also be manually activated through a button on the vehicle operator's remote control console. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

Active Protection System: The Wolverine is equipped with SDI Aegis Active Armor System, a modular, distributed hardkill active protection system designed to protect the vehicle from rockets, missiles, top-attack munitions, and cannon-launched HEAT projectiles. The system consists of a set of pre-warner radar arrays and multiple modular countermeasure modules mounted along the turret sides and roof containing electro-optical tracking sensors and directional explosive countermeasures designed to destroy or deflect oncoming projectiles before they strike the vehicle. The radar tracking system employs eight low-power Ka band (35 GHz) frequency-modulated continuous wave (FMCW) radar panels which detect and track oncoming projectiles at ranges of 10-30 meters from the vehicle. four panels are arranged around the sides of the turret with another two on the turret roof which provide combined 360 degree hemispherical coverage around the vehicle. The short range and low power level of the radar antenna (less than 1 watt each) minimizes the chances the radars will be detected by enemy ECM or electronic intelligence sensors. The radars are used to detect and track incoming projectiles and determine if they are on a course to impact the vehicle. Information from the radar arrays is processed by a central open-architecture countermeasures processor unit which identifies incoming threats and then activates further electro-optical sensors which provide fine tracking of incoming projectiles 2 to 4 meters from the vehicle. Countermeasure initiation is triggered by the electro-optical LADAR sensors with the interception point being approximately a meter from the vehicle. The explosive countermeasures used by the system are contained in bricks on the outside of the vehicle and employ a directional DIME (dense inert metal explosive) charge which fires a blast of micro-sized (1-2mm diameter) hevay metal tungsten alloy (HMTA) shrapnel towards the projectile. The direction of the blast can be steered up or down by varying where the detonation in the charge initiates, allowing the modules placed along the turret to provide coverage over the the hull of the vehicle by steering the blast downwards or to defeat over-fly top attack projectiles by firing upwards. The blast of micro-shrapnel is designed to destroy oncoming threats at distances of a meter or less and loses momentum very rapidly due to air resistance, rendering it safe to dismounted infantry past four or so meters from the vehicle. The countermeasures bricks themselves employ a metal-free composite construction and are encased in a layer of thermoplastic armor to prevent the brick itself from generating any shrapnel and to protect the explosive charges from small arms fire and shrapnel and other hazards. The vehicle by default is fitted with eight countermeasure modules along the sides of the turret which provide coverage around the the hull and turret sides against direct attack or over-fly top-attack projectiles and an additional four roof-mounted countermeasure modules to intercept diving top-attack munitions.


Mobility
  • Name: HL66
  • Type: Multi-fuel diesel engine
  • Length: 830 mm
  • Width: 700 mm
  • Height: 770 mm
  • Dry Weight: 610 kg
  • Bore/stroke: 115/105 mm
  • Displacement, cylinder: 1.1 l
  • Displacement, total: 6.6l
  • Charging method: two-stage variable-geometry turbocharger
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 6, V, 90 degrees
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 550 kW @ 3,800 RPM
  • Torque: 1590 N-m @ 2,300 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The Wolverine employs a conventional rear drive system with a powerpack containing an AMG HL66 six cylinder engine and an AMG AK 6-200 hydrokinetic transmission with six forward and six reverse gears. The air inlets for the engine are on the roof of the engine compartment with the exhaust at the aft. The vehicle's suspension is a semi active in-arm hydro-pneumatic design and consists of six overlapping rubber-tired road wheels on each side of the vehicle which are each connected to a suspension arm with an integral hydro-pneumatic shock absorber.

Engine: The engine used in the vehicle's powerpack is an AMG HL66, a six cylinder, common rail fuel fuel injection, twin sequentially charged low-heat rejection diesel engine which outputs a maximum of 750 PS (550 kW) of power at its maximum rated speed of 3,800 RPM. The HL66 employs a common rail fuel-injection system with a fuel rail running the length of the engine and twin hydraulic boost pumps running at up to 3,100 rpm to pressurize the fuel to 1,800 bar for injection into each cylinder. Turbocharging is accomplished with twin single-stage variable-geometry turbocharger units using variable-area turbine nozzles which providing boost pressure ratios up to 5:1. A water-to-air charge-air cooler is placed after the turbocharger compressor stages to cool and density the air before entering the combustion chambers. To maximize engine performance across a broad ambient temperature spectrum the water and oil cooling system of the engine are split into a high temperature loop which cools the piston liners, cylinder heads, and other engine components along with the first stage of the charge-air cooler, and a low temperature loop which cools the power electronics, engine oil, and the second stage of the charge-air cooler. A dual-circuit water pump circulates cooling water through both the high and low temperature loops and then through the radiator cooling system which employs twin 30 kilowatt variable-speed fans to cool the coolant before it's passed into the expansion tank and then circulated again through the twin coolant loops. An integrated flywheel starter generator is used to start the engine and is rated for mechanical input power of up to 600 kW and outputs 3 phase 60 Hz 600 VAC alternating current. Other engine accessories including inlet air filter system, turbo intercooler and aftercooler circuits, charge air cooler with inlet manifold, exhaust scrubber and infrared suppression system, and oil filter and cooler, are included in the power pack as a single engine unit.

Transmission: The HL66 engine is coupled to an AMG AK 6-200 hydromechanical power shift, reversing and steering transmission which has six forward and six reverse gears. The transmission employs a powershift system with planetary gearing capable of shifting under full engine load, a reversing gear mechanism, and a hydrokinetic torque converter with a lock-up clutch to improve efficiency at higher speeds. Operation of the transmission is fully automatic and automatically changes gear within a range pre-selected by the vehicle operator. A digital transmission control unit (TCU) is used to control shifting in automatic mode which interfaces with the engine control unit (ECU) to control the range of the transmission. The steering drive fitted to the transmission is an infinitely variable hydrostatic/hydrodynamic superimposed differential system employing twin hydraulic drives with variable-displacement hydraulic pumps and twin hydraulic motors which are used to add or subtract power from each side of the vehicle and allow for neutral or pivot turning at infinitely variable speed. Power is transferred to each sprocket using a planetary final drive. Braking functions of the transmission include a combined hydrodynamic/mechanical dual circuit integrated brake system with an internal hydrodynamic brake and external oil-cooled power assisted disc brakes on either side of the transmission. Independent service and parking brakes are additionally included. A hydraulic power take-off (PTO) system fitted to the transmission output is used to power the transmission cooling fans as well the accessory drive gearbox which contains a toroidal CVT (continuously variable transmission) which provides a constant 3,000 rpm speed output independent of engine RPM which is used to drive the vehicle's self-cleaning air filter (SCAF), scavenge blower, and IR exhaust suppression system.

Suspension & Running Gear: The suspension system used by the vehicle is an SDI designed semi-active in-arm hydro-pneumatic suspension system with three sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (12 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable from between 10 and 70 cm depending on terrain with a default of 40 cm. The vehicle's running gear features a decoupled design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle's road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units. Instead of conventional steel tracks the vehicle employs composite rubber band tracks which are 50% lighter and result in a 70% vibration reduction and 10 dB noise reduction inside the vehicle at a road speed of 50 kph. The tracks are 550 mm wide with a 120 mm pitch and have a designed durability of over 5,000 km before needing replacing.


Fire Control & Situational Awareness:
Independent Thermal Sight: The vehicle's primary surveillance and targeting sensor is a two-axis stabilized independent thermal sight which is located on the turret roof. The main features of the sight are a third generation dual-wavelength (3-5 um and 8-14 um) thermal imager and high-resolution color CCD imager with 2-axis independently stabilized line of sight, ballistic computer, eye-safe laser rangefinder, and integrated GPS/inertial navigation system. The third generation thermal imager used with the gunner's sight is a 1280 x 1024 pixel dual color (MWIR and LWIR) capable Mercury cadmium telluride (HgCdTe) staring focal plane array (FPA) detector based system which features an architecture common to several other SDI designed third gen thermal imaging systems. The thermal imager is cooled using a Stirling cycle linear drive cryocooler which cools the detector assembly to 77°K. The detector and crycooler system are contained in a single Standard Advanced Dewar Assembly (SADA), a closed-cycle dewar-cooler assembly containing the linear crycooler, infrared FPA, Dewar, and various control electronics and sensors. The dual-color thermal imager features a color fusion system which assigns colors to pixel values from each MWIR and LWIR band (red for LWIR, cyan for MWIR), adding color contrast to the otherwise black-and-white thermal image. The thermal sight can be toggled between 3x magnification wide field of view (WFOV), 10x magnification medium field of view (MFOV), x25 narrow field-of view (NFOV), and x50 ultra-narrow field of view settings. Mounted alongside the thermal imager is a 1920 x 1080 pixel visible/near IR monochrome CCD camera with selectable 10x NFOV and 3x MFOV optical magnification with additional x25 narrow and x50 ultra-narrow magnification digital zoom capability which provides the sight with an additional daylight channel in addition to the dual-band thermal channel. An image fusion function is also available combines the data from the dual-band thermal imager and the CCD camera to provide a fused image selectable on the sight control panel from 100% visible / 0% IR to 0% visible / 100% IR in infinitely variable increments. Range information for the fire-control system is provided by a 2.06 um holmium-doped YLF eye-safe solid-state laser rangefinder which provides range data accurate to 1 meter from ranges of 80 meters up to 20 kilometers. The sight additionally contains a 1064 nm laser designator, laser illuminator and laser spot tracker. The sight's dual axis stabilized head mirror assembly provides for enhanced on-the-move (OTM) stabilization capability, ensuring the reticle of the sight stays stabilized in the center of the sight while the vehicle is on the move. Dual-axis stabilization is provided by micromachined 2-axis hemispherical Resonator Gyroscopes (HRGs) with 0.001 °/hour drift capability integrated into the sights inertial measurement unit (IMU) system. The sight is further integrated with a GPS/INS navigation system which inputs accurate heading, attitude, velocity and position information of the vehicle into the sight's ballistic computer. The navigation system combines 3 axis fiber optic gyroscopes, 3 axis pendulous accelerometers, and digital magnetic compass with further sensor input from vehicle motion sensor (VMS) systems in the drivetrain and two lightweight, jam resistant DGPS antenna integrated into either side of the sight housing. Attitude information from the GPS is used to give the sight far target location (FTL) capability which combines data from the GPS/INS system and laser rangefinder to provide a complete 3- dimensional attitude solution for the fire control system complete with 10-digit grid coordinate of a target accurate to within several meters at ranges up to 10 kilometers. The sight also includes automatic target recognition (ATR) capability using an imaging sensor autoprocessor (ISA) unit built into the sensor. The ISA employs parallel very high speed integrated circuit (VHSIC) processors contained in a single LRU which includes the video multiplexer, segmentation processor, recognition processor, and and execution controller. Mid-wave and long-wave infrared video output from the FLIR sensor is input into the ISA which then analyses the scene and uses edge detection and parallel processing image recognition algorithms to classify targets based on their size and contrast and attempts to match them with an on-board threat library of targets which includes trucks, armored personnel carriers, tanks, helicopters, and other vehicles. Targets identified by the sight can then be designated and engaged through networked fires from artillery, missiles, aviation, or using the vehicle's own weapons.

Acoustic Gunshot Location System: The turret of the vehicle is fitted with an SDI acoustic gunshot location system (AGLS) which uses a series of microphones to triangulate the location of incoming small arms, cannon, and rocket fire. The AGLS uses an array of four microphones fitted to a mast mounted to the rear of the turret which provides 360° hemispherical coverage around the vehicle. Incoming fire is triangulated to a probable shooter location with +/- 2° azimuth, +/-3° elevation, and +/- 10% range RMS error with the ability to interface with the vehicle's GPS system to provide 10 digit grid coordinates of the shooter probable location. The AGLS also interfaces with the vehicle's fire control system and can automatically slew the turret or RWS in the direction of detected threats.

Missile/Laser Warning System: The vehicle is equipped with a passive missile and laser warning system which provides both warning of incoming threat missiles and illumination by threat lasers. The system employs four optical sensor heads with integral optical signal converters mounted around the turret which provide combined 360° azimuth and −10° to + 45 ° elevation coverage, a central processor which inputs and analyses signals from the four sensor heads to detect and classify threats, and a central control unit located in the vehicle which provides visual and aural threat warning to the crew and allows for control of the system. Each sensor heads contains an ultra-violet (UV) single-pixel quadrant sensors with an adjunct UV sensor for improved dynamic blanking, a laser warning sensor which warns the Operator when the vehicle is being illuminated by a laser designator/illuminator/rangefinder or if the aircraft is being targeted by a laser beam-riding missile, and a short-wave infrared (SWIR) camera which provide detection and tracking of incoming rocket and tracer ammunition. The missile and laser warning system delivers audio and visual warning of detected laser threats through to the operator through the operator control station's intercom system and through the operator control station displays. The system is also integrated into the vehicle's fire control system and features integral counterfire capability where the system can automatically slew the turret to within <2° RMS of detected laser or missile threats through a button on the vehicle operator controller to allow the threat to be rapidly engaged by the vehicle's armament.


Autonomous Navigation & Control:
Autonomous navigation system: The vehicle's autonomous navigation system (ANS) comprises the vehicle's terrain scanning and navigation sensors and terrain perception and path-planning algorithms and is responsible for autonomously driving the vehicle on or off-road between user selected GPS waypoints. The ANS also provides vehicle navigational state data for use by other vehicle systems external to the ANS including the vehicles weapons and surveillance sensors. For detecting terrain the ANS employs four LADAR imaging perception modules (LIPMs) mounted to the front of the hull which each contain a 2-D scanning LADAR (LAser Detection And Ranging) sensor and two pairs of stereo color cameras. The LADAR sensors operate with a 905 nm wavelength at 75 Hz with 0.25°angular resolution and generate a 2D terrain profile along the direction of travel with the ability to detect and image terrain obstacles up to 80 meters from the vehicle. The LADAR sensors are augmented by four sets of stereo camera pairs which uses twin 1024 x 768 pixel CCD cameras with 90° FOV lenses which provide stereo range acquisition of terrain obstacles ahead of the vehicle and when combined with the LADAR sensors provides color 3D imagery of terrain in the direction of travel. The LADAR and stereo camera sensors are coupled to a core navigation system (CNS) module which combines a differential GPS (DGPS) receiver with <2 cm navigation accuracy and a 9-axis inertial measurement unit combining 3-axis fiber optic gyro, 3-axis accelerometer, and 3-axis magnemometer and a navigation computing system (NCS) module which contains a 933 MHz processor with 256 MB of memory which provides sensor-fusion of LADAR and stereo camera imagery and runs the terrain perception and path-planning algorithms necessary for autonomous off-road navigation. The terrain perception algorithm is responsible for fusing the imagery produced by the LADAR and stereo camera systems in order to determine the exact location of terrain obstacles or other terrain hazards in the vehicle's direction of travel. LADAR data is combined with stereo camera imagery to generate colorized LADAR data which is then combined with positional data from the INS/GPS navigation system in order to geolocate each pixel in the colorized LADAR data with respect to the vehicle's coordinate frame. The terrain perception logarithm also includes a slope estimator algorithm which uses an estimation of the ground surface curvature in front of the vehicle in order to detect slopes that are too steep for the vehicle to climb, a ditch estimator designed to detect depressions in the ground, and object height estimator which determines the height of objects in front of the vehicle. The path-planning algorithm is used alongside the terrain perception algorithm to travel between GPS waypoints when navigating autonomously. Using the path-planning algorithm the vehicle will attempt to navigate in a straight line between GPS waypoints at a specified speed dependent on the terrain roughness, using the terrain perception algorithm to scan along the vehicle's current direction of travel for any potential obstacles or terrain hazards. Should the terrain perception algorithm detect a hazard such as obstacle in the vehicle's path which is too tall to climb over, a slope too steep for the vehicle to climb or drive across, or a ditch too wide for the vehicle to cross the vehicle will reduce its speed and the path-planning algorithm will attempt to navigate the vehicle around the obstacles or terrain hazard by using an active contour model to "snake" around the obstacles or terrain hazard.

Operator Control Station: The Wolverine is controlled via an operator control station (OCS) located inside a manned armored vehicle which consists of three large multifunction touchscreen displays with bezel buttons for display and crewstation control and a video game console handheld controller used for remote vehicle control and target acquisition. Each multifunction touchscreen display can be used to display two different information displays including the driving display, control display remote sensor feed, mission planning information, and digital terrain map displays. In teleoperation mode video feed from the vehicle's driving cameras is streamed at a rate of 1-10 Mbps and is displayed in the center multifunction display. Data from the terrain perception algorithm is also overlaid onto the camera feed in order to warn the operator of any terrain obstacles in the vehicle's current path. Below the camera feed are four dials which display the vehicle's current speed, azimuth, pitch, and roll. As a way to prevent the operator from inadvertently flipping the vehicle the pitch and roll dials will flash red if the vehicle's pitch or roll exceeds 30°. The top right of the driver's display is used to display an overhead digital terrain elevation map of the area around the vehicle. The display will also alert the operator if the vehicle's fault detection system detects a fault in the vehicle through a flashing warning at the bottom of the display. The control display is used to control the vehicle's various operational modes and functions. In autonomous navigation mode the touschscreen display is used to plan routes using digital terrain maps of the area and to generate the GPS waypoints that the vehicle will follow when navigating autonomously. The display also acts as a vehicle health monitoring display and will display the the location, type, and consequences of detected faults in addition to the warning message that appears in the driving display.

The handheld controller is modified from a commercial video game console controller and is used for both driving and for sensor and weapon control under teleoperation mode. When driving the vehicle the right joystick is used to steer the vehicle while the left joystick is used to control the vehicle speed. When driving one or both triggers (L1 or L2) must be continuously depressed, ensuring that the vehicle will come to a stop if the operator drops or looses control of the controller. When operating the turret or FLIR sensor the left joystick is used to control traverse, the right joystick used to control elevation, and the triggers used to control camera zoom. The vehicle cam be controlled from the operator control console in four different modes; teleoperation mode, autonomous mode, vehicle leader-follower, and dismount leader-follower mode. In teleoperation mode the imagery and navigation data from vehicle's cameras and INS/GPS are streamed to a operator workstation in near-real time and the vehicle is steered remotely by the user using the hand held controller. In teleoperation mode a wireless LAN radio 2.4 GHz omni-directional datalink antenna with a UDP-based data transfer protocol is used to exchange data between the control station and vehicle which limits data transfer rate to 10 kbps for steering and control commands, 60 kbps for telemetry and 10 Mbps for video feed. An additional emergency stop radio (ESR) independent of the wireless LAN radio is also included in the communications system which acts as an independent 'kill switch" to trigger system shutdown in both teleoperation and autonomous operation modes. In teleoperation mode should the vehicle loose radio contact with the control station it will enter a 'standby' mode, remaining still until control can be re-established. In autonomous mode the user selects one or more GPS waypoints using the control display which the vehicle will then drive to while autonomously detecting and avoiding any obstacles along the route. In vehicle leader-follower or “robotic convoy" mode the Wolverine can be instructed to follow either a manned vehicle or another Wolverine which it will attempt to follow at a specified distance using it's forward imaging perception sensors. Should the follower vehicle lose track of the 'leader' vehicle the follower will revert to GPS navigation using GPS waypoints received by the leader vehicle. Dismount leader-follower is identical to vehicle leader-follower except the vehicle is instructed to follow a walking person rather than a vehicle.
Last edited by The Technocratic Syndicalists on Mon Sep 20, 2021 7:21 pm, edited 29 times in total.
SDI AG
Arcaenian Military Factbook
Task Force Atlas
International Freedom Coalition


OOC: Call me Techno for Short
IC: The Kingdom of Arcaenia

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The Technocratic Syndicalists
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Postby The Technocratic Syndicalists » Sat Nov 13, 2021 6:13 pm

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PzBfw 303

General Characteristics:
  • Type: Armored command vehicle
  • Weight: 31.0 t
  • Length: 6.8 m
  • Width: 3.4 m
  • Height: 2.4 m
  • Crew: 2 (driver, commander) + 5 staff officers or system operators

Mobility:
  • Engine: 2x AMG HL44 multi-fuel twin-turbo V4 diesel engines, 400 kW (550 PS) each
  • Transmission: Diesel-electric; 2x 300 kW traction motors, 2x 150 kW steering motors
  • Suspension: Active in-arm hydropneumatic
  • Max onroad speed: 75 km/h
  • Max offroad speed: 60 km/h
  • Max reverse speed: 30 km/h
  • Fuel capacity: 950 l
  • Operational range: 750 km

Armament:
  • 1x 8 mm MG-45E, 1,000 rounds

Maneuverability:
  • Power/weight Ratio: 37.0 PS/t (26.7 kW/t)
  • Ground clearance: 0.50 m
  • Ground pressure: 0.70 kg/cm2
  • Gradient: 60%
  • Sideslope: 40%
  • Fording depth: 1.5 m
  • Trench crossing: 2.6 m
  • Vertical wall climb: 1.0 m


Overview
The Panzerbefehlswagen 303 (PzBfw 303) is a command and control vehicle designed by SDI vehicle systems which is designed to act a mobile command post at the division, brigade, and battalion level. The vehicle is a variant of SDI's PzKfz 303 Marten armored personnel carrier and consists of a PzKfz 303 chassis and drivetrain fitted with a raised superstructure to give the inside of the vehicle more working room for command and control operations.


Armament
Scanfire RWS: For self defense the vehicle is fitted with an SDI Scanfire remotely operated weapon station. The Scanfire weighs 140 kg and and includes an electro-optical sensor suite with a daylight CCD camera, uncooled 640 x 480 pixel LWIR (long wave infrared) infrared imager, and eye-safe Nd:YAG laser rangefinder along with an MG 45E machine gun and an ammunition box containing 1,000 rounds of 8x57 mm ammunition. The Scanfire features dual-axis gyro-stabilization and 360° traverse at 90 °/s and -20° to +70° elevation at 60°/s using brushless DC servomotors. In addition to the MG 45E the Scanfire can mount other machine guns from 7.62 mm to 12.7 mm caliber or 40mm automatic grenade launchers. Ammunition capacity is 1,000 rounds for 7.62mm machine guns, 500 rounds for 12.7 mm machine guns, and 60 rounds for 40mm automatic grenade launchers.


Protection:
Armor Protection: The hull of the vehicle is constructed from friction stir welded (FSW) 2139-T8 aluminum alloy plates 40 mm thick which provides the hull 360° protection against 14.5 mm AP ammunition at 200 meters and 155 mm high explosive shell fragments at 30 meters. The base armor is augmented by ceramic armor panels containing tandem silicon-carbide (SiC) tiles embedded into a cast 7075 alloy aluminum matrix which along with the base armor provide frontal arc protection (+/- 30°) against 30 mm APFSDS rounds at 500 meters and 360° protection against 152 and 155 mm high explosive shell fragments at 10 meters. The inside surface of the vehicle features a borated spall liner consisting of orthogonally cross-plied M5 ballistic fibers laminated into a flexible borated polyethylene resin which serves to minimize the post-armor effect of penetrating projectiles and shaped charge jets and to provide radiation protection for the crew and electronics inside the vehicle. Under-belly protection is provided by an armored V-hull which provides protection against EFPs and 10kg TNT equivalent blast anti-tank mines. Additionally the four vehicle crew members located in the hull sit on blast-attenuating seats with no direct contact to the vehicle floor.

Fire extinguishing system: The crew, fuel, and powertrain compartments of the vehicle include an automatic fire suppression system (AFSS) which is designed to prevent fires inside the vehicle caused by penetrating munitions. Combined UV/IR electro-optical infrared sensors placed inside the crew and ammunition compartments and are used to detect the formation of explosive fires inside the vehicle within several milliseconds. The engine, transmission, and fuel compartments of the vehicle substitute the electro-optical sensors with several loop of thermal sensing wire. When a fire is detected inside the vehicle Halon 1301 contained in several pressurized bottles each with fast-reacting solenoid-actuated valves is sprayed into the compartment to extinguish the fire. After the compartment is flooded with halon and the fire extinguished the vehicle's ventilator is automatically switched on and the residual smoke and halon gas is then vented to the atmosphere.

NBC System: The vehicle's NBC systems consists of pressure swing adsorption (PSA) system which supplied filtered air to the crew compartment and maintains fighting compartment pressure at a constant 4 millibar above outside atmospheric pressure. The pressure swing adsorption (PSA) system works by using two filter beds' one adsorbing at high pressure while the other is regenerating at low pressure by the removal of previously adsorbed particles. Following regeneration the incoming air is diverted to the cleaned bed and the bed previously on line begins its regeneration cycle. Air first is drawn into the system through a cyclone filter which removes dust and biological particles from the air before it enters the first stage air compressor. The first stage air compressor raises the air pressure to 1.8 bar where the air is then cooled by passing through the first stage heat exchanger before it enters the second stage air compressor. The second stage air compressor raises the air pressure to 3.0 bar where the air is again cooled by passing it through the second stage heat exchanger. The air then enters the on-line bed where it is cleaned . The cleaned air that leaves the on-line bed is cooled by passing it through a recuperator where it is then expanded through a turbine which drives the second stage air compressor. The cold air leaving the turbine is released into the crew compartment through a pressure relief valve (PRV) which maintains the crew compartment at 4 millibar above outside atmospheric pressure.


Propulsion
  • Name: HL44
  • Type: Multi-fuel diesel engine
  • Length: 890 mm
  • Width: 450 mm
  • Height: 740 mm
  • Dry Weight: 450 kg
  • Bore/stroke: 115/105 mm
  • Displacement, cylinder: 1.1 l
  • Displacement, total: 4.4l
  • Charging method: two-stage variable-geometry turbocharger
  • Intercooling: Air-oil aftercooler
  • Number of Cylinders: 4, inline
  • Cooling method: Water cooled
  • Injection method: Common rail, piezoelectric direct injection
  • Specific fuel consumption: 190 g/kW-hr
  • Power: 400 kW @ 4,300 RPM
  • Torque: 920 N-m @ 3,800 RPM
  • Fuel: JP-5, JP-8, Ultra-low sulfur diesel
The vehicle employs a diesel-electric drive system consisting of twin diesel engines and integrated starer/generator units places in the hull sponsons and a mechanically regenerated hybrid electro-mechanical cross-drive transmission located in the front of the hull which combines the power input of the traction and steering motors and distributes it to the twin drive sprockets. The mechanical decoupling of the diesel engines with the drive sprockets allows for the engines to run at a constant RPM, improving fuel efficiency, while the use of two diesel propulsion units and twin steering and traction motors in the transmission provides a high level of redundancy and resistance to damage. The packaging of the diesel engines in the hull sponsons also serve to increase the effective internal volume of the hull for crew, weapons, and other payload.

Engine: The engine used in each powerpack is an AMG (Arkaenisch Motorenfabrik Gesellschaft) HL44, a four cylinder inline, common rail fuel fuel injection, twin sequentially charged low-heat rejection diesel engine which outputs a maximum 400 kW of power at 4,300 rpm. The engine also includes an integral oil-cooled permanent magnet synchronous flywheel starter-generator unit which is geared to the engine output shaft using a speed-increasing transfer case with a fixed 4.2:1 gear ratio. The HL44 employs a common rail fuel-injection system with a fuel rail running the length of the engine and twin hydraulic boost pumps running at up to 3,100 rpm to pressurize the fuel to 1,800 bar for injection into each cylinder. Turbocharging is accomplished with twin single-stage variable-geometry turbocharger units using variable-area turbine nozzles which providing boost pressure ratios up to 5:1. A water-to-air charge-air cooler is placed after the turbocharger compressor stages to cool and density the air before entering the combustion chambers. To maximize engine performance across a broad ambient temperature spectrum the water and oil cooling system of the engine are split into a high temperature loop which cools the piston liners, cylinder heads, and other engine components along with the first stage of the charge-air cooler, and a low temperature loop which cools the power electronics, engine oil, and the second stage of the charge-air cooler. A dual-circuit water pump circulates cooling water through both the high and low temperature loops and then through the radiator cooling system which employs twin 30 kilowatt variable-speed fans to cool the coolant before it's passed into the expansion tank and then circulated again through the twin coolant loops. An integrated flywheel starter generator is used to start the engine and is rated for mechanical input power of up to 400 kW and outputs 3 phase 60 Hz 600 VAC alternating current The starter-generator is a self-excited, brushless, oil cooled, permanent magnet machine using neodymium-iron-boron permanent magnets and has a rated speed of 18,000 RPM, necessitating a 4.2:1 gear ratio speed-increaser gearbox be placed between the generator and engine. Other engine accessories including inlet air filter system, turbo intercooler and aftercooler circuits, charge air cooler with inlet manifold, exhaust scrubber and infrared suppression system, and oil filter and cooler, are included in the power pack as a single engine unit. The left and right hand side powerpacks are identical and can be fitted to either side of the vehicle. The powerpack additionally includes the oil cooling system with air-oil heat exchanger and a hydrostatically driven cooling fan.

Transmission: The vehicle powertrain system employs a mechanically regenerated cross-drive transmission which reduces the required motor power required to drive and regeneratively brake each drive sprocket. The transmission system includes twin 150 kilowatt oil-cooled permanent magnet synchronous steering motors and twin 300 kilowatt oil-cooled permanent magnet synchronous traction motors located on either sides of the transmission. Both traction and steering motors employ a rotor with samarium-cobalt magnets and a ferromagnetic core with an inconel superalloy sleeve and have a maximum rated speed of 18,500 RPM with a 93% efficiency at a base speed of 4,600 RPM. The steering and traction motors on either side of the transmission are supplied electrical power through a generator converter box located in each sponson ahead of the the powerpack which converts the three phase 600 volt AC power from the engine generators into 600 volt DC power which is transferred to a DC bus located on either side of the cross drive unit which then supplies DC power to the motor inverters and the various accessory drives. The cross drive unit itself contains a central drive shaft connected to a differential gearbox which combines the inputs from the two steering motors and two traction motors to power the drive sprockets through the planetary reduction final drive assemblies located on either side of the cross-drive transmission. A two speed oil-cooled planetary reduction gearbox with twin hydraulically actuated clutches is additionally incorporated into the cross-drive transmission and connects the central differential to the steering and traction motors to reduce the required rpm and torque ranges of the electrical steering and traction motors. The cross drive additionally contains an oil cooled wet disk brake and a parking brake unit.

Suspension & Running Gear: The suspension system used by the vehicle is an SDI designed semi-active in-arm hydro-pneumatic suspension system with three sets of paired, overlapping 800 mm diameter rubber-tired road wheels on either side of the chassis (12 road wheels total) each mounted on a swing-arm with an integral in-arm suspension unit (ISU) which allows for independent control of each road wheel bogie. Each ISU consists of a compressed nitrogen shock absorber and hydraulic dampener unit contained inside the roadwheel arm. When the arm rotates upward a piston-arm attached to a stationary pivot is forced into a cylinder in the moving suspension arm which in turn displaces the hydraulic fuel inside and compresses the nitrogen gas inside, causing the unit to act as a spring. The variable damping of the suspension is provided by a stack of hydro-mechanically controlled wet friction discs located on the hull pivot axis of the in arm suspension unit which are compressed by a hydraulic pressure plate to vary the dampening rate of the suspension arm as a function of the suspension arm position and velocity. Ground clearance of the vehicle is adjustable by the driver from between 100 and 700 mm, depending on terrain. The vehicle's running gear features a decoupled design where the final drives and sprockets, idlers, and roadwheel arms are all mounted on left and right side running gear carriers which are decoupled from the sides of the hull using rubber mounts. The vehicle's road wheels employ a twin hollow shell design formed using twin hollow cavities constructed from a single 7075-T6 aluminum alloy forging fitted with an inner steel wear ring and polyurethane tire which are then bolted together back-to-back to form the complete road wheel units. Instead of conventional steel tracks the vehicle employs composite rubber band tracks which are 50% lighter and result in a 70% vibration reduction and 10 dB noise reduction inside the vehicle at a road speed of 50 kph. The tracks are 550 mm wide with a 120 mm pitch and have a designed durability of over 5,000 km before needing replacing.


Variants:
PzBfw 303:Standard Command and control variant which is intended to act as a mobile command post at the division, brigade, and battalion level. The vehicle is equipped with a complete C4I (Command, Control, Communication, Computer and Intelligence) with HF, VHF and UHF radios as well as broadband satellite communication system. The vehicle also includes an erectable tent with 12 m2 of floor space which can be deployed in around 20 minutes with 2 soldiers to provide additional work space. Armament consists of an SDI Scanfire remote weapon station carrying a machine gun or automatic grenade launcher.

FltPzA 303: Artillery fire direction variant of the PzBfw 303. The FltPzA 303 is fitted with mission computers running the SDI Wotan Fire Support System (FSS) and provides command, control and data processing for artillery batteries equipped with the AtKpfw 173 self propelled howitzer.

FltPzM 303: Mortar fire direction variant of the FltPzA 303. Like the FltPzA 303 the FltPzM 303 is equipped with mission computers running the SDI Wotan Fire Support System (FSS) and provides command, control and data processing for mortar companies equipped with the GwKpfw 303 self propelled mortar.

SKfz 303: Ambulance and medical treatment variant of the PzBfw 303 which can be configured either as an ambulance or medical treatment vehicle. As an ambulance the vehicle has a crew of 3 and can carry 6 ambulatory patients, 4 litter patients, or 3 ambulatory patients and 2 litter patients. As a medical treatment vehicle the vehicle has a crew of 4 with the ability to carry 1 litter patient and includes an erectable treatment shelter, various medical equipment including vital signs monitor and defibrillators, and a refrigerator for storing blood.
Last edited by The Technocratic Syndicalists on Sat Nov 13, 2021 7:15 pm, edited 5 times in total.
SDI AG
Arcaenian Military Factbook
Task Force Atlas
International Freedom Coalition


OOC: Call me Techno for Short
IC: The Kingdom of Arcaenia

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