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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:03 pm

moved for renovations
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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:05 pm

moved for renovations
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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:10 pm

moved
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NW Canadian Aerospace-Transport Aircraft

Postby United NW Canada » Sat Nov 20, 2010 11:13 pm

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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:22 pm

moved for renovations
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NW Canadian Aerospace-EW & Recon Aircraft

Postby United NW Canada » Sat Nov 20, 2010 11:33 pm

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NW Canadian Aerospace-Support Aircraft

Postby United NW Canada » Sat Nov 20, 2010 11:34 pm

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NW Canadian Aerospace-Naval & Maritime Aircraft

Postby United NW Canada » Sat Nov 20, 2010 11:36 pm

CSV-22 Sea Lion ASW V/STOL Aircraft
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Submarines only die tired trying to run from this Sea Lion!

The CSV-22 Sea Lion ASW V/STOL Aircraft is a tilt-rotor aircraft with both a vertical takeoff and landing (VTOL), and short takeoff and landing (STOL) capability. It is designed to combine the functionality of a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft. identify and have the ability to track, and destroy enemy submarines, surface craft and land targets.The CSV-22 Sea Lion ASW V/STOL Aircraft is an all-weather, multi-mission aircraft with long range, which is capable of extended missions with in-flight refueling.

For finding its targets the CSV-22 Sea Lion possesses an advanced and integrated systems of sensors that combine Thermal, Optical, ESM, Radar, Magnetic Anomaly Detection, and both Active and Passive Sonar. The Sea Lion also mounts on its fuselage a AN/AAQ-33 Sniper pod. The Sniper ATP incorporates a multi-spectral sensor capability with a high-resolution, mid-wave third-generation FLIR and a CCD-TV. Advanced sensors, combined with advanced image processing algorithms and rock-steady stabilization produce target identification ranges that permit operations minimizing exposure to many threat systems. The dual-mode laser offers an eye safe mode for urban combat and training operations, along with a laser-guided bomb designation laser for guiding in these precision munitions.

Tactically, the CSV-22 Sea Lion mounts a 0.50cal GAU-19 mini-gun in a remote retractable mount under the nose of the aircraft. The main weapons bay is of an modular design (9800 lb/4455 kg capacity) and can carry a variety of bombs, depth charges, and missiles.

The CSV-22 Sea Lion can also function in the role of Tanker aircraft. The Sea Lion possesses a retractable refueling drogue under the base of the tail section. The internal Weapons bay is plumbed to accept a 4000 Liter fuel module. Fuel can be transferred from the Sea Lion's own internal tanks or the fuel module to refuel other aircraft. The fuel module can be used to triple the range of the Sea Lion at the expense of a weapons payload.

Cost:$ 35,000,000.00
Class: Anti-submarine V/STOL Aircraft
General characteristics
* Crew: Four (pilot, copilot and two sensor/weapons operators)
* Length: 57 ft 4 in (17.5 m)
* Rotor diameter: 38 ft 0 in (11.6 m)
* Wingspan: 45 ft 10 in (14 m)
* Width with rotors: 84 ft 7 in (25.8 m)
* Height: 22 ft 1 in/6.73 m; overall with nacelles vertical (17 ft 11 in/5.5 m; at top of tailfins)
* Disc area: 2,268 ft² (212 m²)
* Wing area: 301.4 ft² (28 m²)
* Empty weight: 33,140 lb (15,032 kg)
* Loaded weight: 47,500 lb (21,500 kg)
* Max takeoff weight: 60,500 lb (27,400 kg)
* Powerplant: 2× Rolls-Royce Allison T406/AE 1107C-Liberty turboshafts, 6,150 hp (4,590 kW) each

Performance
* Maximum speed: 250 knots (463 km/h, 288 mph) at sea level / 305 kn (565 km/h; 351 mph) at 15,000 ft (4,600 m)[131]
* Cruise speed: 241 knots (277 mph, 446 km/h) at sea level
* Range: 879 nmi (1,011 mi, 1,627 km)
* Combat radius: 370 nmi (426 mi, 685 km)
* Ferry range: 1,940 nmi (2,230 mi, 3,590 km) with auxiliary internal fuel tanks
* Service ceiling: 26,000 ft (7,920 m)
* Rate of climb: 2,320 ft/min (11.8 m/s)
* Disc loading: 20.9 lb/ft² at 47,500 lb GW (102.23 kg/m²)
* Power/mass: 0.259 hp/lb (427 W/kg)

Armament
* 1× 0.50cal GAU-19 mini-gun, belly-mounted, retractable, video remote control in the Remote Guardian System
* Up to 9800 lb (4455 kg) in modular internal weapons bay

Avionics
* AN/APS-137 Inverse Synthetic Aperture Radar, maximum range 150 nmi (173 mi, 278 km)
* OR-89 forward looking infrared (FLIR) camera with 3x zoom
* AN/AAQ-33 Sniper pod, fuselage mounted
* AN/ARS-2 sonobuoy receiver with 13 blade antennas on the airframe for precise buoy location (Sonobuoy Reference System)
* AN/ASQ-81 magnetic anomaly detector (MAD)
* AN/ASN-92 inertial guidance system with doppler radar navigation and TACAN
* OASIS III (Over-the-horizon Airborne Sensor Information System)
* AN/AQS-13F dipping sonar
* ALE-39 countermeasure system (90 rounds of chaff, flares, and expendable jammers)
* Sonobuoy Dispenser (59 tactical, 1 Search and Rescue)
Last edited by United NW Canada on Sun Dec 05, 2010 8:28 pm, edited 4 times in total.

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NW Canadian Aerospace-Attack Helicopters

Postby United NW Canada » Sat Nov 20, 2010 11:38 pm

CBA609 Kestrel Attack Tilt Rotor (release soon!)
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CAH-24 Super-Hind (Sea Hind)

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Bigger than most other gunships, the bulky CAH-24 Super-Hind carries a large weapon loud out of cannons, rockets and anti-tank missiles. The Hind is also able to carry up to 8 troops or 4 stretchers in the med-evac role. With the NW Canadian Forces, this helicopter is used in an Air Cavalry role, supporting Special operations, and by NW Canadian Marines.

The CAH-24 Super-Hind Hind sacrifices maneuverability for speed and survivability. The helicopter's large wings not only provide plenty of space for rockets and missiles but also provide some much needed lift for the heavy Hind. The Hind holds the world speed record for active military helicopters.

CAH-24 Super-Hind are built around core digital systems which integrate flight, sensor and combat systems together. The integrated avionics system (IAS) includes two mission computers and an automatic flight control system. Each crew station has two 8x6-inch multifunction liquid crystal displays (LCD) and one 4.2x4.2-inch dual function LCD display. The communications suite combines RT-1824 integrated radio, UHF/VHF, COMSEC and modem in a single unit. The navigation suite includes an embedded GPS inertial navigation system (EGI), a digital map system and a low-airspeed air data subsystem, which allows weapons delivery when hovering.

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The CAH-24 Super-Hind features a stabilized nose-mounted sensor/sight package featuring FLIR, range finder, TV camera, and Laser designator. Targeting unit and cannon are both slaved to the crews helmets and control of each can be selected or shared.

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CAH-24 Super-Hind is a very survivable aircraft. The Rotor Blades are made of composites, which have an increased ballistic survivability, and there is a semiautomatic folding system for stowage aboard ships. The rotor blades also have anti-ice protection to allow operations in arctic environments. The engines are equipped with engine exhaust suppressors to reduce IR signature. Along this vein the aircraft is also equipped with IR jammers and the ALE-47 “Smart” Countermeasures Dispenser. To warn the crew that aircraft is being targeted it is equipped with AVR-2A Laser Warning Receivers, APR-39A(v) 2 Radar Warning Receivers and the AAR-47 Missile Warning Device.

The body is heavily armored and can resist impacts from .50 caliber (12.7 mm) rounds from all angles, including the Composite rotor blades. The cockpit is an even more heavily armored titanium tub and can resist impact from 37mm cannon rounds. The cockpit and crew compartment are over pressurized to protect the crew in NBC conditions.

Cost: $40,000,000.00
General characteristics
* Crew: 2-3: pilot, weapons system officer and technician (optional)
* Capacity: 8 troops or 4 stretchers
* Length: 17.5 m (57 ft 4 in)
* Rotor diameter: 17.3 m (56 ft 7 in)

* Wingspan: 6.5 m (21 ft 3 in)

* Height: 6.5 m (21 ft 3 in)
* Disc area: 235 m² (2,530 ft²)
* Empty weight: 8,500 kg (18,740 lb)
* Max takeoff weight: 12,000 kg (26,500 lb)
* Powerplant: 2× Isotov TV3-117 turbines, 1,600 kW (2,200 hp) each

Performance
* Maximum speed: 335 km/h (208 mph)
* Range: 450 km (280 miles) on internal fuel
* Service ceiling: 4,500 m (14,750 ft)

Armament
Internal guns
* flexible 25mm dual feed auto-cannon with 1200 (600/600) rounds of ammunition
* 2 x 7.62mm machine guns mounted on passenger compartment doors.

External stores
* Total payload is 1,900 kg of external stores.
* Inner hardpoints can carry at least 500 kg; plumbed for drop tanks
* Outer hardpoints can carry up to 250 kg
* Wing-tip pylons can carry quad pods of ATGWs or AAMs

Bomb-load
* Bombs within weight range up to 500 kg.
* MBD multiple ejector racks (presumably MBD-4 with 4xFAB-100)
* KGMU2V submunition/mine dispenser pods
* MU90 Impact homing torpedoes
* CFGUV-8700 gunpod (with a 12.7 mm + 2x7.62 mm combination or one 40 mm Striker AGL)
* UB-32 CRV7 rocket launchers (CRV-7 unguided rockets, and CRV-7PG Laser guided rockets)
* Quad pack: 9K121 Vikhr ATGW
* Quad pack: Brimstone ATGW
* Quad pack: Hellfire
* Multi pack: 8 x CRV-7PG, 2 x Brimstone/Hellfire/9K121 Vikhr
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* Quad pack: 9K338 Igla-S AAMs
* Quad pack: FIM-92A Stinger Blk II AAMs
* Dual pack: Python-5 AAMs
* Kh-25MP (AS-12 'Kegler')-all variants








CAH-64N Sea Apache
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The Sea Apache is different from the normal AH-64 series in many ways. One of the major differences between the CAH-64 Sea Apache and US AH-64 variants is the folding blade mechanism to stow the helicopters in confined spaces; the rotor blades also have anti-ice protection to allow operations in arctic environments. Another is the use of Rolls-Royce Turbomeca RTM322 01/12 engines instead of the General Electric T700-GE-701Cs. The Rolls-Royce engine produces 1,565 kW (2,100 hp) vs 1,410 kW (1,890 hp) for the GE T700C engine. Also there are increased corrosion preventive measures, improved electro-magnetic interference protection, a Doppler navigation system, upgraded brakes, additional tie down points, and a powered automatic rotor blade fold system.

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There are changes to the sensor and avionics outfitting the craft as well; connectivity with the BOWMAN secure communications system to interact with other units being a significant one. SELEX (formerly BAE Systems Avionics) Helicopter Integrated Defensive Aids System (HIDAS) were also fitted.

Like the US AH-64D Apache Longbows; the CAH-64 Sea Apache carries a fire-control radar (FCR) and Radar Frequency Interferometer (RFI), providing an integrated surveillance and attack system. The 'Longbow’ radar is the bulbous unit over the rotor hub assembly; radar placement above the rotors allows the Apache to hover behind cover scanning for targets, with only the radar unit exposed


Cost: $40,000,000.00
General characteristics
* Crew: 2
* Length: 17.7 m (58 ft 4 in with rotors turning)
* Rotor diameter: 14.6 m (48 ft)
* Height: 3.87 m (12 ft 8 in)
* Disc area: 168.11 m² (1,809.5 ft²)
* Empty weight: 5,165 kg (11,387 lb)
* Loaded weight: 8,006 kg (17,650 lb)
* Max takeoff weight: 9,525 kg (21,000 lb)
* Power-plant: 2× Rolls-Royce/Turbomeca RTM322 turbo-shaft, 1,566 kW (2,100 hp) each

Performance
* Never exceed speed: 365 km/h (197 knots, 227 mph)
* Maximum speed: 293 km/h (158 knots, 182 mph)
* Cruise speed: 259 km/h (140 knots, 161 mph)
* Range: 1,700 km (1,121 mi)
* Service ceiling: 6,400 m (21,000 ft)
* Rate of climb: 12.7 m/s (2,500 ft/min)

Armament
* Guns: M230 Chain Gun, 1156 rounds
* Missiles: Hellfire, Brimstone, Stinger, Starstreak, Sidewinder/Sidearm, Harpoon, Penguin, Python-5
* Rockets: CRV7 (Flechette (Tungsten dart) or High-Explosive Incendiary Semi-Armour Piercing (HEISAP))
Last edited by United NW Canada on Sun Jan 09, 2011 10:17 pm, edited 8 times in total.

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NW Canadian Aerospace-Transport Helicopters

Postby United NW Canada » Sat Nov 20, 2010 11:54 pm

(Show Room Under Construction)
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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:55 pm

moved for renovations
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moved for renovations

Postby United NW Canada » Sat Nov 20, 2010 11:58 pm

moved for renovations
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NW Canadian Weapon Systems-Pistols and PDWs

Postby United NW Canada » Sat Nov 20, 2010 11:58 pm

NW Canadian Weapon Systems1
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NW Canadian Weapon Systems-Rifles and Shotguns

Postby United NW Canada » Sat Nov 20, 2010 11:59 pm

CM-109 Heavy Sniper/Anti-Material Rifle

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The CM-109 is an anti-materiel rifle, chambered in 25 x 59 mm.

The CM-109 is a semi-automatic anti-materiel rifle, designed primarily for engagement of light armored vehicles and similar material targets. It is also very effective against personnel based targets.

The 25 x 59 mm cartridge is used in the CM-109 and the CM307. The CM-109 offers greater range and a shorter overall length than the previous 0.50 caliber systems, as well as potentially greater power in the 25 x 59 mm cartridge over even the Mk 211 .50 BMG cartridge (aka "Raufoss round"). For some long-range sniper missions, a .50 caliber (12.7mm) round just isn’t big enough.

Specifications
Weight 33.2 lb (15 kg) empty, without scope
Length 46 inches (1168 mm)
Barrel length 17.5 inches (44.45 cm)
Cartridge 25 x 59 mm
Action Semi-Automatic
Muzzle velocity 425 m/s (1,390 ft/s)
Effective range 2,000 m (1.2 mi)
Maximum range 3,600 m (2.2 mi)
Feed system 5-round detachable box magazine


Designed to destroy light armor, the CM-109 is a semi-automatic 25mm rifle that has a 17.6 inch long barrel and an overall length of 46 inches. It weighs in at 46 pounds and has a 5 round magazine. In comparison, the Barrett M107 .50 caliber sniper rifle in general use today has a 29 inch barrel, overall length of 57 inches, and weighs in at a mere 32 pounds, with a magazine capacity of 10 rounds.

To complement this “rifle” is a computerized sight called the ORS (Optical Ranging Sighting System). ORS is specifically designed for long-range shooting at 1,000 meters and longer distances, measuring and compensating for air pressure, temperature, and the angle of the weapon in relation to the target. Precisely compensating for all these factors and successfully hitting the target on the first shot is possible, but difficult. BORS is designed to take all the sweat-math work out of first-round shots, leaving the operator with simply dialing in the distance to target, selecting the ammunition type, and putting the cross-hairs on the target. Future versions of BORS will incorporate a rangefinder, and night vision capability.

A spiked bipod is included to steady the CM-109 for firing and it has a standard M1319 accessory rail for scopes and other accessories. It also has the ability to remove the muzzle break and replace it with a specially designed sound suppressor.

Effective distance armor piercing “lethality” for the rifle is listed at 2000 meters. The 25mm round is derivative design from the AH-64 Apache helicopter’s M789 high-explosive dual purpose (good against armor and personnel) 30mm ammunition and will penetrate at least 50 millimeters of armor plating, making it capable of destroying light armored vehicles, SCUD launchers, and other equipment. The 25mm round is 2.5 times more effective at destroying targets than a .50 caliber armor-piercing round.
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NW Canadian Weapon Systems-Squad Automatics & Machineguns

Postby United NW Canada » Sat Nov 20, 2010 11:59 pm

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The CGPMG-1A1 General Purpose Machine Gun

The CGPMG-1A1 is a gas operated, air cooled, belt fed General Purpose machine gun that is in widespread service with the NW Canadian Military.

Caliber: 7,62x51mm NATO (Standard, other available. See below)
Weight: 8.2 kg (18.26 lb) empty; on bipod
Length: 1040 mm (Standard Barrel), 887 mm Commando Barrel) with stock fully collapsed
Barrel length: 502 mm (Standard Barrel), 349 mm (Commando Barrel)
Feed: belt
Rate of fire: selectable: 650,750, and 950 rounds per minute


Action:
The CGPMG-1A1 is a gas operated, belt fed, air cooled machine gun. It fires from an open bolt and has a quick detachable barrel. The gas system consists of a gas chamber with a manual gas regulator, and a long stroke gas piston located below the barrel.

Locking is achieved through a rotating bolt with dual locking lugs. Firing as from open bolt, the action provides selective fire capability through three-position manual safety-fire selector, located on the left side of the pistol grip. The belt feed unit is installed on the top of receiver, with belt feeding direction from left to right. Belt feed is operated by the side-mounted swinging lever, which is operated by cam track cut in the side of the bolt carrier. The ejection window for empty cases is at the right side of receiver, just below the empty link ejection window.

The CGPMG-1A1 machine gun utilizes long-stroke gas piston system located below the barrel. Gas system is fitted with three-position gas regulator, with first (minimum) position used to fire when fed from magazines, second when firing from belts in normal conditions and third – when firing belts under adverse conditions. The gas regulator setting also affects the cyclic rate of fire (position #1 – lowest rate, #3 – highest). The gas piston is attached to the bolt group by dual operating rods, running at either side of receiver.


Chambering:
The CGPMG-1A1’s standard chambering is for the venerable 7.62x51mm round (7.62 Nato). The modular construction allows for a variety of calibers with the change of the upper assembly and barrel.
Other calibers which the CGPMG-1A1 is currently offered are:
7.62x54mmR
7.92x57mm Mauser
.303 British (7.7x57mmR)
.30-06 (7.62x63mm)
7.5mm French


Feed:
Gun is fed using standard disintegrating belts. The belts are usually fed from semi-rigid “assault pouches” with 150- or 200-round capacity. These pouches are clipped to machine gun below the receiver, using special projection at the top which is inserted into magazine housing and locked there using magazine catch. Loading and ejection windows in the feed unit have spring-loaded dust covers which automatically open and close during each reloading cycle. The feed unit cover is hinged at the front and can be lifted up for loading, unloading or inspection.


Barrel:
Barrel is quick-detachable barrel with two barrel sizes available –Standard (long) and Commando (short). Barrel locking is achieved by rotating the bolt with four massive radial lugs which engages the cuts in the breech of the barrel.

It is interesting to note that when fitted with short (Commando) barrel, and with bipod removed, the CGPMG-1A1 represents a formidable and effective CQB weapon, providing high maneuverability in confined spaces, with added benefit of serious firepower, thanks to its relatively heavy and quick-changeable barrel. The issues of length issues are further aided by the weapon’s adjustable stock.


Sighting:
The CGPMG-1A1 is fitted with backup aperture sights, and has a Picatinny rail on the top of the receiver, and three on the fore grip that can accept wide variety of sights and accessories.

The CGPMG-1A1 is equipped normally with the NWC79 Optical Sight of 3.4x28 magnification. A tritium-illuminated reticle provides for normal and low-light conditions sighting. The NWC79 differs from the standard 3.4x sight in that ballistic compensation is provided for in the reticle, rather than in the mount. Reticle illumination is by a battery-powered LED with eleven intensity settings. The scope itself is Nitrogen-purged to prevent fogging and is covered with an armored coating of rubber. The reticle of the NWC79 sight was designed for service on Machine Guns, thus an appropriate pattern was chosen to aid the gunner in judging distance. The reticle consists of a single vertical post with a sharp tip in the center. The tip is flanked by horizontal Mil-bars on either side. Under the left-hand Mil-bar, a second horizontal bar was added for judging distances.


Features:
The standard butt stock the CGPMG-1A1 is a telescoped 5 position adjustable stock. This allows the weapon to be configured both for the Firer, but also the tactical situation. In its shortened position it aids in maneuvering the weapon in tight confines.

The feed channel rail, feed link, both feed slides and the feed tray are chrome plated. The top cover body is an anodized aluminum casting. This provides a very high degree of resistance to dirt and the elements and aids in maintaining the weapon.

As standard, the CGPMG-1A1 has a modular pistol fore-grip with integral tactical illumination laser light mounted to the rail beneath the fore barrel/ gas system. This is to aid in the use of the CGPMG-1A1during assault operations. It provides the firer more control of the weapon when firing on the move or from a non-prone position as well as a source of illumination if required, as well as aiding accuracy for quick, close-in engagements. This unit can be removed or replaced as needed.

A lightweight detachable folding bipod is attached to the gas tube of the CGPMG-1A1. The weapon can be mounted as well, on vehicles and infantry tripods for sustained or long range fire missions. It is also can be used as a co-axial weapon in vehicle systems.

Pricing:
The Pricing for the CGPMG-1A1 is variable depending on the relations of the Nations wishing to purchase and the number of weapons said nation wishes to purchase.

For accurate up to date pricing please contact NW Canadian Defense Solutions and a purchasing package can be put together especially for your Nation.
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NW Canadian Weapon Systems-Crew Served Weapons

Postby United NW Canada » Sun Nov 21, 2010 12:00 am

NW Canadian Weapon Systems4
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NW Canadian Weapon Systems-Anti Tank Weapons

Postby United NW Canada » Sun Nov 21, 2010 12:01 am

M83A2 SLADAR (Shoulder-Launched Active-homing Disposable Anti-tank Rocket)

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The M83A2 SLADAR (Shoulder-Launched Active-homing Disposable Anti-tank Rocket) is a lightweight one-shot anti-armor weapon capable of engaging enemy vehicles at ranges up to 1,000 m. Fully disposable, the rocket's launcher is discarded after firing, whilst the rocket, a fire-and-forget weapon, guides itself toward the target. When stowed, the SLADAR system consists of a watertight carbon-fiber composite blast tube, inside of which is an aluminum launch tube containing the missile and guidance electronics. The weapon is cocked by unlatching the forward ring of the blast tube and pulling the inner launch tube forwards until it locks. A trigger assembly and thermal acquisition sight are then flipped into position, and the weapon activated by pushing a charge button on the trigger grip. From this point the weapon can be sighted and fired from the shoulder.

The M83 acquires and tracks targets with a cooled infrared imaging seeker mounted in the rocket's nose. When the charge button is pressed, the inert IR seeker is cooled to its operating temperature within two seconds and begins feeding images to the operator's thermal acquisition sight. The seeker remains charged for twenty minutes, after which the rocket may only be fired unguided. When a target (such as a vehicle) enters the acquisition sight, the operator can lock the seeker onto the target. So long as the target image remains clearly within the seeker's field of view, the weapon can be launched at it.

When launched, the SLADAR rocket accelerates to maximum velocity. As the rocket approaches the target, the guidance system selects the hottest part of the target (on a tank, usually the weakly protected engine deck) and flies an attack profile that offers optimum penetration. Against a tank, it will typically climb briefly before diving on the target's thinner upper surfaces. The M83A2 version is capable of identifying defensive countermeasures such as decoy flares and has improved logic to aid in rejecting them. The shaped-charge HEAT warhead is capable of defeating most light and medium armor. Penetration of RHA: 600mm

Since SLADAR is an open-chambered weapon, operators must allow for back blast. The rear of the blast tube is packed with small plastic slivers which fire backward on launch of the rocket and absorb much of the back blast. A cleared back blast zone of 10 meters behind the weapon is recommended, and care should be taken in launching the rocket from confined spaces.

SLADAR may be fired unguided like an RPG, using a backup reticule sight to aim. This is commonly done in the field against objects like bunkers, pillboxes, crew-served weapons, supply dumps and communications centers - all of which do not give off a characteristic thermal signature. Though the rocket still has a maximum range of about 1,000 m against these targets, unguided aiming is not accurate beyond 200 m.

Cost: $3,000.00 USD

M83A2 SPECIFICATION

Length (closed) 64 cm
Length (firing position) 90 cm
Weight 3.1 kg
Minimum Range 20 m
Maximum Range 1,000 m
Penetration of RHA: 600mm



M112 HIMAT (Hypervelocity Intelligent Missile, Anti-tank)


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The HIMAT (Hypervelocity Intelligent Missile, Anti-tank) is a man-portable "brilliant" weapon with a range greater than 5 km.

An extremely versatile weapon, it gives commanders many options for deployment and use.

The main element is an 11.3 kg single-shot, self-contained, disposable launcher equipped with bipod and baseplate. The bipod can be set for any angle between 0 and 90 degrees.

Defensive use-When used defensively, the HIMAT can be set for "Command" or "Automatic". In either case, one or more launchers are connected via cables to the Fire Control Unit, an intelligent computer system which receives data from the local sensor matrix, including motion trackers, IR scanners, LIDAR, RADAR, and robotic sentries. The FCU can also be linked to command-wide units such as surveillance drones, forward observers, or satellites. The FCU analyses all available sensor data and upon positively identifying a threat, it will lock on with one or more missiles and prepare to launch.

The next action depends on whether the FCU is set to "Command" or "Automatic". In "Command" mode, an operator constantly monitors the designated anti-tank area. When a threat is identified, the FCU will show a "Target Lock", allowing the operator to either authorize a missile launch or request further IFF (Identification, Friend or Foe) interrogation. In "Automatic" mode, the FCU will work through it's target ID protocols to ensure it has identified an enemy, then it will automatically launch one or more missiles.

Offensive use-The HIMAT can be used in direct fire mode by plugging an infantry SR-90 Target Acquisition Sight into the launcher. The SR-90 combines passive IR with an active millimeter wave radar motion tracker and has enough cable to distance the operator up to 150m away from the launcher. Once the operator has a target locked-on, the information from the sensors is passed to the missile, which is launched by the operator.

HIMAT missile-The missile itself is a small two-stage round with a multi-sensor seeker. Upon launch, the missile is ejected from it's tube vertically by the first-stage motor where it's control vanes orient it towards the target. The second-stage then fires, accelerating the missile nearly instantaneously to Mach 4.5. The seeker consists of a millimeter-wave radar and an aerial that allows "home-on-jam" capabilities. The seeker scans the target during it's approach and determines it's exact type and configuration from memory. If the target turns out to be friendly, the missile will steer itself away and self-destruct. If the target is hostile, the seeker will determine the optimum impact point and steer the missile towards it.

The warhead is comprised of a 15 cm tungsten rod surrounded by high explosive. The explosive is detonated just before impact, launching the rod into the target's armor, similar to a tank SABOT round. The combination of the missile's hypervelocity and the explosive force allows the tungsten rod to penetrate all but the strongest armor. Penetration of RHA: 900mm

The HIMAT has some success against aerial targets, such as low-flying UAVs, helicopters, and VTOL aircraft. A multi-purpose warhead is being designed for use against both ground and aerial targets.

Cost: $10,000.00 USD
Last edited by United NW Canada on Mon May 23, 2011 3:59 am, edited 3 times in total.

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NW Canadian Weapon Systems-Incendary & Explosive devices

Postby United NW Canada » Sun Nov 21, 2010 12:01 am

NW Canadian Weapon Systems6
Last edited by United NW Canada on Sun Nov 21, 2010 1:04 am, edited 1 time in total.

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Air Defense Systems

Postby United NW Canada » Sun Nov 21, 2010 12:01 am

C9K38 Needle MANPAD

Image

Image

The NW Canadian C9K38 Needle is a man-portable infrared homing surface-to-air missile (SAM).

The development of the Needle short-range man-portable air defense system (MANPADS) began with the main goals to create a missile with better resistance to countermeasures and wider engagement envelope than the earlier MANPADS systems.

Technical difficulties in the development quickly made it obvious that the development would take far longer than anticipated however,

The Needle features an optional Identification Friend or Foe system to prevent firing on friendly aircraft, an automatic lead and super elevation to simplify shooting and reduce minimum firing range, a slightly larger rocket than most MANPADS, reduced drag and better guidance system extend maximum range and improve performance against fast and maneuverable targets, an improved lethality on target achieved by a combination of delayed impact fuzing, terminal maneuver to hit the fuselage rather than jet nozzle, an additional charge to set off the remaining rocket fuel (if any) on impact, an improved resistance to infrared countermeasures (both decoy flares and ALQ-144 series jamming emitters), and slightly improved seeker sensitivity.

Tests have shown the Needle to be superior over the contemporary but smaller and lighter American FIM-92A Stinger missile. The Needle possess a high degree of resistance against flares and jamming, a more sensitive seeker, expanding forward-hemisphere engagement capability to include straight-approaching fighters (all-aspect capability) under favorable circumstances, a slightly longer range, a higher-impulse, shorter-burning rocket with higher peak velocity (but approximately same time of flight to maximum range), and a propellant that performs as high explosive when detonated by the warhead's secondary charge on impact.
Cost: $30,000.00 per unit

Specifications
Weight,full system: 19 kg (42 lb)
Weight, missile alone 11.7 kg (26 lb)
Length 1.574 m (5.16 ft)
Diameter 72 mm

Warhead 1.17 kg (2.6 lb) with 390 g (14 oz) explosive
Detonation mechanism contact and grazing fuzes

Engine solid fuel rocket motor
Operational range 5.2 km (3.2 mi)

Flight ceiling 3.5 km (11,000 ft)
Speed 800 m/s (peak), about Mach 2.3
Guidance system two color infrared
Last edited by United NW Canada on Tue Mar 01, 2011 5:33 pm, edited 2 times in total.

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moved for renovations

Postby United NW Canada » Sun Nov 21, 2010 12:02 am

moved for renovations
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NW Canadian Weapon Systems

Postby United NW Canada » Sun Nov 21, 2010 12:57 am

aaaaa
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