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The Marquesan Armed Forces Aircraft Commission (Do Not Post)

A place to put national factbooks, embassy exchanges, and other information regarding the nations of the world. [In character]
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Marquesan
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The Marquesan Armed Forces Aircraft Commission (Do Not Post)

Postby Marquesan » Thu Sep 17, 2020 10:22 am


Image
Artwork by Lauzanne.

Nomenclature: LFI.16/1R4 "Super Revenant"
Classification:
Lightweight Fighter / Interceptor

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
May 13th, 2005

Program Cost:
14,790,000,000 NSD

Number Built:
4,930


Specifications:

Crew:
1 (Pilot)

Overall Length:
18 meters (59')

Tail Height:
5.26 meters (17'4")

Wingspan:
9.84 meters (32'3")

Wing Area:
46.40 m2 (499.45 ft2)

Wing Loading:
358.18 Kg/m2 @ MTOW (73.36 Lbs/ft2)

Empty Weight:
7,436 Kgs (16,394 Lbs)

Internal Fuel:
8,815.7 liters - 7,184 Kgs (15,838 Lbs)

Gross Weight:
14,620 Kgs (32,231.6 Lbs)

Payload Capacity:
2,000 Kgs (4,409.25 Lbs)

Max Takeoff Weight:
16,620 Kgs (36,641 Lbs)

Powerplant:
1x MTV45.112R Thrust Vectoring Turbofan

Rated Thrust:
112.23 kN @ Military Power, 170.65 kN @ Reheat

Thrust-to-Weight Ratio:
1.04:1 @ MTOW (kgf:kg)

Fuel Burn:
2.0 Kg/Sec @ Supercruise, 7.0 Kg/Sec @ VNE

Performance:

Takeoff & Landing Performance:
Takeoff in 610 meters (2,000') @ 280 Km/H, (174 MPH) Landing in 880 meters (2,890') @ 160 Km/H (99.4 MPH)

Supercruise Performance:
1,830 Km (1,137.1 miles) in 58 Minutes, 43 Seconds @ 1,870 Km/H (Mach 1.51)

Maximum Performance: (VNE - above 10,000 meters / 32,808')
750 Km (466 miles) in 17 Minutes @ 2,635 Km/H (Mach 2.14)

Service Ceiling & Climb Rate:
21,340 meters (70,013') in 72 Seconds @ 300 M/Sec (59,055 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLF "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 1x AC22.L82/2 Dual-barrel autocannon @ Right Wingroot w/ 1,050 Rds

Hardpoints:
x6; 1 Wingtip, 2 Underhung per wing + 8 Internal

Typical Combat Load:
1,600 kgs missiles & bombs + 400 kgs ammunition

- 6x AHM.210R2 "Bayonet" Heat-Seeking AAMs (External)

- 2x MHL.201R2 "Fire Lance" Radar-Homing AAMs (Wingtips)

- 8x S-UMP-100 "Kisten" Small-Diameter Bombs (Internal)

Description:

The first-generation Revenant fighter first took flight in 2013 in the now-abandoned region of Sondria. Revenant was rushed into service by Forces Marquises aux Armes, and over the course of years, has undergone several major and minor updates during its lifetime. Major revisions in 2020 and late 2022 saw enhancements like refinements in sensors and armaments, and an up-engine from a low-bypass turbofan to a much more powerful mid-bypass afterburning turbofan. The latest Revision 4, equipped with the MTV45.112R turbofan is referred to as "Super Revenant" due to the mild chassis stretch the aircraft underwent to accommodate the new engine. The stretched R4 Super Revenant is only 59 feet in length and weighs less than half of the maximum takeoff weight of the twin-engine Divine Wind fighter; a wingspan of only 32 feet allows for Super Revenant units to be diffused out to tiny installations where they will be required to operate from disguised hangars on public roads, taking off in only 2,000 feet and landing in slightly more. Moderate wing loading and a 1.04:1 thrust to weight ratio allow for razor-sharp maneuvers and extreme accelerations; a 59,000 foot per minute climb rate is nearly unmatched among light fighters. Super Revenant's intended role is as a point defense interceptor and dogfighter, optimized to operate in a supersonic regime to an intercept point, and then to dogfight using a powerful array of weapons, including a dual-barrel 22mm autocannon mounted at the right wingroot, the high-speed heat seeking Bayonet missile, and radar homing Fire Lance missiles. Super Revenant's semi-low observable design and diminuitive size lower an enemy's detection window for Super Revenant, often bringing the fighter inside air-to-air kill range with Bayonets before being discovered. Super Revenant is rated to operate as high as 70,000 feet and has just under an hour of fuel for supercruising at military power with the afterburner off at Mach 1.5 and much longer at lower throttle positions. External and internal hardpoints carry a mix of weapons, with a typical combat loadout including eight Lauzannean "Kisten" small-diameter guided glide bombs, allowing LFI.16/1R4's to operate as true all-weather multirole fighters carrying out pinpoint ground strikes as well as defending friendly airspace.

Super Revenant fighters fly with a sophisticated electronics package that uses compact, modular systems common to other Marquesan aircraft and fighting systems, referred to as Testudo Mk. IV. The 2020 revision of the Mk. III System includes a modern, low-power X-Band radar, which simultaneously scans vertically and horizontally at 30 Hz. The extremely sensitive Rigel radar can detect the smallest RCS targets at ranges of up to 60 kilometers, and produces swift, stable radar locks for the Fire Lance missile the fighter carries on its wingtips. The inverse-monopulse Fire Lance missile uses the latest jamming-hardened, high speed communications to seek targets using the agile radar onboard the Super Revenant. The Rigel radar can track 400 targets simultaneously and produce dozens of simultaneous missile locks. A sophisticated "Aquila" is a small optronics blister, located on the upper side of the nosecone forward of the cockpit. The Aquila EOTS blends the inputs of a dual band Mid & Long-Wave Infrared sensor with a 10 Megapixel visible light camera, both sensors attached to a power telephoto zoom lens with up to 40x magnification. This all-weather system corrects for atmospheric interference such as smoke, dust or rain, allowing the Super Revenant pilot to not only fly but perform in adverse conditions. The Rigel radar and Aquila optronics pod work together to identify and discriminate targets automatically for the pilot, but can also produce live "false daylight" full color thermal vision with blended radar overlays, so that a pilot could see through a rainstorm to identify an armored vehicle on the ground under the cover of foliage, or identify a hostile fighter flying at night, beyond normal visual range and confirm the make of the aircraft and any external armament it was carrying with a minute risk of detection given the long range of the Bayonet missiles carried and the rapid seek rate of the short range, radar guided Fire Lance missiles. A Timing & Inertial Measurement Unit, or TIMU continuously self-calibrates the aircraft's location in relation to predetermined waypoints in the aircraft's mission plan, considered 99.85% accurate even in commuication or GPS-denied environments, the aircraft's computer provides turn-by-turn directions to the crew. If the aircraft is connected to the encrypted SANMEN communications network, mission parameters such as waypoints, targets, etc. can be changed in flight and updated to allow forces to rally or regroup instaneously.

Real World Comparison - - SAAB JAS 39 "Gripen": R4 Super Revenant is longer than Gripen by about two meters, with one meter wider wingspan and a nearly-identical maximum takeoff weight. Super Revenant's wing area is higher than Gripen, so Gripen's wing loading number is higher, making a less maneuverable aircraft with higher takeoff and landing speeds than Super Revenant. The Marquesan fighter's MTV45.112R turbofan produces roughly twice the thrust than the General Electric RM16 despite not being massively larger due to technological development since Gripen's design process began. Revenant is slightly faster at top speed, and Gripen's useful payload is higher because the amount of fuel it carries is much lower than Super Revenant, which allows the Marquesan fighter to stay aloft longer at higher speeds and fuel consumption rates than Gripen, while Gripen carries more ordnance aloft. Super Revenant's higher thrust and lower wing loading allow for a much higher ceiling, beating Gripen's maximum altitude by more than six kilometers. A lower-RCS shape for Super Revenant and modern sensor suite with long range weapons compound Super Revenant's advantages in a hypothetical engagement, being able to engage the Swedish fighter from outside its detection range and from significantly above its service ceiling.

Flyaway Cost Per Unit:(Place orders Here.)
55,000,000 NSD.

Research Links:
Last edited by Marquesan on Mon Nov 13, 2023 6:49 am, edited 55 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Marquesan
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Civil Rights Lovefest

ADF.36/1R5 "Divine Wind"

Postby Marquesan » Thu Sep 17, 2020 2:53 pm


Image
Artwork by Lauzanne.

Nomenclature: ADF.36/1R5 "Divine Wind"
Classification:
Air Dominance Fighter

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
February 8th, 2005

Program Cost:
68,620,000,000 NSD

Number Built:
730

Specifications:

Crew:
1 (Pilot)

Overall Length:
21.10 meters (69'3")

Tail Height:
4.55 meters (14'11")

Wingspan:
13.70 meters (44'11")

Wing Area:
80.30 m2 (864.34 ft2)

Wing Loading:
450.80 Kg/m2 @ MTOW (92.33 Lbs/ft2)

Empty Weight:
16,630 Kgs (36,663 Lbs)

Internal Fuel:
16,652.3 liters - 13,570 Kgs (29,917 Lbs)

Gross Weight:
30,200 Kgs (66,580 Lbs)

Payload Capacity:
Internal Ordinance - 6,000 Kgs (13,328 Lbs)

Max Takeoff Weight:
36,200 Kgs (79,807 Lbs)

Powerplant:
2x MTV45.112R Thrust Vectoring Turbofans

Rated Thrust:
112.23 kN @ Military Power, 170.65 kN @ Reheat each

Thrust-to-Weight Ratio:
0.96:1 @ MTOW (kgf:kg)

Fuel Burn:
1.20 Kg/Sec @ Supercruise, 5.72 Kg/Sec @ VNE

Performance:

Supercruise Performance:
4,900 Km (3,044.70 miles) in 3 Hours, 10 Minutes @ 1,560 Km/H (Mach 1.26)

Maximum Performance: (VNE - above 10,000 meters / 32,808')
1,600 Km (994 miles) in 39 Minutes, 30 Seconds @ 2,430 Km/H (Mach 1.96)

Service Ceiling & Climb Rate:
20,000 meters (65,616') in 63 Seconds @ 315 M/Sec (62,007 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aLF "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Hardpoints:
2x Internal Carousels for x4 Missiles each

Typical Combat Load:
2,960 Kgs (6,526 Lbs) Ordinance

- 4x OGM.189R2 "Misericorde" Heat-Seeking Missiles

- 4x RHM.147R2 "Corseque" Radar-Homing Missiles

Description:

Divine Wind was the first truly modern Marquesan fighter to take flight in the early 2000's, a replacement for Cold War-era Type-410 and Type-408 fighters nearing their retirement ages. A process of constant refinement and revision has yielded five major design iterations of the Divine Wind fighter. The latest version, currently in service with Forces Marquises aux Armes and many allies and customers abroad, is Revision 5. Just over 69 feet in length and with a wingspan of just under 45 feet, Divine Wind R5 weighs just over 79,800 pounds fully loaded, including 13.5 tons of jet fuel and 6,000 kilograms of internally-carried ordinance. A pair of MTV45.112R afterburning mid-bypass turbofans power the fighter, the same powerplant in service with "Super Revenant" "Headhunter" and "Blackheart" combat aircraft. Each engine produces more than 170 kilonewtons of thrust at afterburner, affording a class-leading 0.96:1 thrust-to-weight ratio, measured at maximum takeoff weight. Divine Wind's intended role is as an Air Dominance Fighter, able to enforce No-Fly zones with high-speed, long range missiles. Divine Wind R5 supercruises at Mach 1.26 at military power, with more than three hours of supersonic endurance at this speed. With afterburners lit, the aircraft is capable of Mach 1.96 and can continue at afterburner for nearly 40 minutes before expending its internal fuel, traveling nearly a thousand miles in that time. The ADF.35/1R5 fighter is built around its central, internal weapons bay, which carries a typical loadout of four (4) "Corseque" Active Radar Homing missiles and four (4) "Misericorde" Heat-Seeking Missiles in a carousel behind the cockpit. Because all weapons are carried internally and antennas are recessed from the surface of the skin to preserve the aircraft's stealthy shape, the R5 Divine Wind has higher performance, longer range and lower RCS than previous versions of the fighter. The fighter's two mid-bypass MTV45.112R turbofan engines are on either side of the weapons bay, just aft of the aircraft's center of rotation. A long and wide blended wing and fuselage body with widely-spaced serpentine ducts places diverterless, fixed-geometry supersonic inlets underneath the wings, which completely obscure the turbine bypass fans from radar. The blended wing/body design allows areas of the fuselage to generate lift, so smaller clipped delta wings with reverse trailing edge sweep merging into leading edge extensions are used, reducing supersonic drag without compromising trans-sonic lift-to-drag characteristics. The airframe incorporates substantial area ruling to reduce aerodynamic drag and maximize acceleration at trans-sonic speeds. The leading and trailing edges of the wings and control surfaces are carefully angled to reduce the number of directions radar waves can reflect. Leading edges and skin surfaces subject to aerodynamic and engine heat are electrically cooled by computer to manage the infrared cross-section of the Divine Wind fighter. The nose section is chiseled with the cockpit placed high to produce excellent visibility for the pilot, and a frameless canopy incorporating coatings that minimize the radar return of the cockpit and protect the pilot from the impact of ultraviolet and thermal radiation. An all-moving V-tail is angled 50° from vertical; pitch is provided by rotating the V-tail fins in opposite directions so the front edges move together or apart; yaw is supplied by rotating the tail fins in the same direction. Raising the wing flaps and ailerons on one side and lowering them on the other provide roll, while deflecting the wing flaps down, ailerons up and V-tails inward provides aerodynamic braking.

The ADF.35 is very agile, with excellent instantaneous and sustained turn performance, high-alpha capability and a general resistance to spins. The supermaneuverable fighter aircraft is still controllable at angles of attack exceeding 60° and can sustain 10-g maneuvers due to the high-instability design. The aircraft has a high fuel load for a fighter its size, is midair-refueling capable and reportedly has easy, "carefree" handling due to computer-controlled thrust vectoring. ADF.35/1R5 is less reliant on radar absorbent materials than other designs to produce a low radar cross-section; the fighter may operate from flight lines rather than climate controlled hangars, and its electrothermally cooled skin elements reduce the aircraft's infrared signature dramatically, especially at supersonic speeds. The "Aruna" Electro-Optical Targeting System retracts into the nose when not in use, further reducing the aircraft's infrared and radar cross-sections, and the aircraft's flat thrust-vectoring nozzles further reduce infrared emissions of the exhaust plume to mitigate the threat of infrared homing ("heat seeking") surface-to-air or air-to-air missiles. Divine Wind's superior high-alpha flight characteristics, 300 meter per second climb rate and 1.01:1 thrust to weight ratio at maximum takeoff weight are kept in check by a full-authority computer management system, making Divine Wind departure-resistant and highly maneuverable in pitch and yaw, and enabling the aircraft to perform acrobatic maneuvers along with flat rotations with very little altitude loss. In previous generations of the Divine Wind fighter, engineers found that pilots failed to maintain active control of the aircraft at high angles of attack due to the ineffectiveness of flight control surfaces at trans-sonic speeds, so full computer control of all flight surfaces by optical cable and full time thrust vectoring for stability was a base requirement of the R5 program. Stability in flight is provided by vectoring the jet exhausts by computer control in sync with the aircraft's Timing & Inertial Management Unit, which adjusts thrust vectoring parameters in real time, up to 50 times per second. Its powerful Netane Kinetics turbofans enable a Mach-1.96 maximum speed and Mach 1.26 supercruise without the use of engine reheat, representing a significant kinematic advantage over many contemporary fighters, with many engine parts coated in high-temperature ceramics to reduce thermal transfer to the airframe. Engine exhausts use three carbon/carbon paddles in the exhaust path to direct engine exhaust up to 30° off boresight; this system operates autonomously of pilot control, reducing workload and continually optimizing thrust and fuel consumption protocols with thrust vectoring and flight control surfaces to match pilot inputs rather than relying on the pilot to operate controls in the cockpit.

Divine Wind's all-glass cockpit features a sweeping, full-color multifunction AMOLED display which surrounds the pilot's field of view. The multifunction cockpit display is interactive with pilot voice commands and with ocular sensors and accelerometers on the pilot's helmet, displaying the most critical information on the pilot's Helmet-Mounted "Augmented Reality" display, projecting images directly onto the pilot's retinas. The highly advanced Aquila optronics suite provides a blister above the nosecone forward of the radar housing a visible light sensor and a Mid & Long-Wave Infrared dual-band sensor together with a 40x telephoto power-zoom lens, allowing the optics to be zoomed coherently by the pilot to identify targets at great distance. These sensors provide infrared search and track, target identification and discrimination, and stunning high-definition false color daylight thermal vision in real time for instrument-only flying conditions. below the nose, a blister is provided for the laser suite, allowing Divine Wind to identify laser spots, to provide laser rangefinding, 3D laser scanning of surface targets and to direct coded laser-guided munitions onto their targets. Forward of the Aquila system is the ring-mount for the Higih-Power X-Band "Altair" radar. The latest advances in compact, EMP-hardened microprocessors and compact solid-state power systems have produced an extremely compact 15-kilowatt radar. The Altair radar has a 110 degree field of view through its radome, and can detect air targets at distances as great as 400 kilometers. Four beams scan the X-band at pseudorandom frequencies simultaneously, producing extremely clear, crisp radar images and updating up to 600 simultaneous tracks at 45 Hz. The Altair radar has an extremely low probability of intercept despite its massive power and long range, permitting the launching aircraft to scan wide swaths of airspace in a combat mission, detecting targets far outside traditional engagement ranges and firing very high-speed, beyond visual range missiles into the targets without ever exposing the fighter, even in extremely poor weather conditions. A Timing & Inertial Measurement Unit, or TIMU continuously self-calibrates the aircraft's location in relation to predetermined waypoints in the aircraft's mission plan, considered 99.85% accurate even in commuication or GPS-denied environments, the aircraft's computer provides turn-by-turn directions to the crew. If the aircraft is connected to the encrypted SANMEN communications network, mission parameters such as waypoints, targets, etc. can be changed in flight and updated to allow forces to rally or regroup instaneously. A complex life support system includes an onboard oxygen generation system, protective pilot garments and a breathing regulator/anti-G valve controlling flow and pressure to the pilots mask and garments. Pilot garments protect against chemical/biological hazards and cold-water immersion, counter g-forces and low pressure at high altitudes, and provide thermal regulation. The canopy includes a Flexible Linear Shaped Charge embedded within the canopy itself. This system is initiated when the eject handle is pulled, and shatters the canopy over the seat a few milliseconds before the seat is launched. A Zero/Zero ejection seat is fitted, allowing for both low-altitude, low altitude ejections and supersonic ejections.

Real World Comparison - - Lockheed Martin F-22 "Raptor": Divine Wind R5 is longer than Raptor by two meters, with similar wing area and wingspan, while ADF.36 has a slightly higher maximum takeoff weight. Divine Wind carries more fuel internally than Raptor, while Raptor's overall payload is higher, with external hardpoints designed to carry ordinance on the wings, which Divine Wind lacks. While wing loading numbers are similar for both aircraft, Divine Wind is designed to carry its ordinance internally, while F-22 carries some ordinance or fuel tanks on the wings, increasing its radar cross section over Divine Wind. Raptor is capable of Mach 2.25 sprints, besting the rated top speed for Divine Wind, however ADF.36's supercruise and maximum performance ranges are dramatically longer than F-22, permitting much longer missions conducted much further from land bases. Additionally, Divine Wind is rated for carrier flight, which F-22's have not been optimized for, a major advantage in hypothetical placement of 5th generation fighters. F-22 carries a cannon where ADF.36 does not, however Misericorde and Corseque missiles dramatically outperform AMRAAM and Sidewinder missiles in similar mission roles.

Flyaway Cost Per Unit:(Place orders Here.)
135,000,000 NSD.

Research Links:
Last edited by Marquesan on Mon Nov 13, 2023 6:15 am, edited 46 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
Kraven Prevails!

User avatar
Marquesan
Minister
 
Posts: 2247
Founded: Oct 21, 2010
Civil Rights Lovefest

PSI.43/2R4 "Headhunter"

Postby Marquesan » Sat Sep 19, 2020 9:36 am


Image
Artwork by Lauzanne.

Nomenclature: PSI.43/2R4 "Headhunter"
Classification:
Penetration Strike/Interdictor

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
February 3rd, 1979

Program Cost:
65,600,000,000 NSD

Number Built:
820

Specifications:

Crew:
2 (Pilot, Weapons Officer)

Overall Length:
24.00 meters (78'8.9")

Tail Height:
5.60 meters (18'4.4")

Wingspan:
15.90 meters (52'2")

Wing Area:
86 m2 (925.7 ft2)

Wing Loading:
497.67 Kg/m2 @ MTOW (101.9 Lbs/ft2)

Empty Weight:
18,170 Kgs (40,058 Lbs)

Internal Fuel:
18,689.2 liters - 15,230 Kgs (33,576.4 Lbs)

Gross Weight:
33,400 Kgs (73,634.4 Lbs)

Payload Capacity: (8x External / 4x Internal Hardpoints)
9,400 Kgs (20,723.4 Lbs)

Max Takeoff Weight:
42,800 Kgs (94,357.8 Lbs)

Powerplant:
2x MTV45.112R Thrust Vectoring Turbofans

Rated Thrust:
112.23 kN @ Military Power, 170.65 kN @ Reheat each

Thrust-to-Weight Ratio:
0.81:1 @ MTOW (kgf:kg)

Fuel Burn:
1.21 Kg/Sec @ Supercruise, 8.46 Kg/Sec @ VNE

Performance:

Supercruise Performance:
4,900 Km (3,044.71 miles) in 3 Hours, 30 Minutes @ 1,410 Km/H (Mach 1.14)

Maximum Performance: (VNE - above 10,000 meters / 32,808')
1,400 Km (869.91 miles) in 30 minutes @ 2,800 Km/H (Mach 2.27)

Service Ceiling & Climb Rate:
21,175 meters (69,472') in 85 Seconds @ 250 M/Sec (49,213 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aLF "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Description:

Project Headhunter sought to develop an agile moderate-weight tactical bomber capable of Mach 2 sprints and carrying a powerful suite of missiles and bombs. The finished aircraft, now in its fourth major revision, is built on a 925 square foot delta wing, with a single vertical tail and recessed S-duct intakes for the type's pair of MTV45.112R mid-bypass afterburning turbofans. Headhunter is designed to be launched from steam catapults on carrier decks, and is the Forces Marquises aux Armes mainstay for combat strike missions. The aircraft is just under 80 feet in length, with a maximum takeoff weight of over 94,000 pounds; it carries fifteen tons of internal fuel and has twelve hardpoints for 9.4 tons of internal and external ordinance. PSI.43's have excellent thrust-to-weight ratio for their class, measured at maximum takeoff weight, of 0.81:1, and exhibit a 49,000 foot per minute climb rate to their 69,000 foot ceiling. At military power, Headhunter supercruises with fuel for three and a half hours of endurance at Mach 1.14, during which time the aircraft can cover move than three thousand miles. With both engines at full reheat, (afterburner) PSI.43 is capable of 870 mile, Mach 2.27 dashes lasting thirty minutes, flying above a 32,000 foot minimum. Headhunter carries a state-of-the-art avionics suite, complete with wraparound glass-panel cockpit displays for the Pilot and WSO. A fly-by-light fiber optic communication suite has four levels of built-in reduncancy, ensuring that flight controls remain functional in the event of damage in flight. Inertial navigation is highly accurate and satellite-independent, the same encrypted SANMEN communication system utilized by other Marquesan combat vehicles and vessels allows Headhunter crews to communicate with allies easily, the network automatically shifting transmission frequencies depending on the sender and receiver by adjusting a compact solid-state plasma antenna onboard the aircraft. The canopy is protected from ultraviolet and thermal radiation, and coated to minimize radar reflections in the cockpit.

As in other Marquesan combat aircraft, the nose of the aircraft houses the Aquila Optronics suite, with an above-nose blister housing a dual-band M/WIR sensor and high-definition visible light sensor aligned together on a 40x telephoto power zoom lens. Stunning clarity is produced with automatic image correction to remove the effects of smog, haze, heavy cloudcover, rainfall, dust or oil smoke. Full-color "false daylight" thermal vision allows for perfect clarity during instrument-only flight conditions for the pilot, increasing situational awareness by color-correcting the night sky and ground below the aircraft for the multifunction in-cockpit display. The below nose blister houses a laser targeting suite including a laser warning receiver, laser rangefinder and coded laser designator, in addition to a 3D laser scanning array to produce precise measurements of targets on the surface. Under the radar-transparent nosecone is housed an extremely modern Altair X-band radar. The latest advances in compact solid-state power systems and EMP-hardened system-on-chip computing have produced an extremely compact 15-kilowatt radar with a 110 degree field of view and 400 kilometer maximum detection range. The Altair radar scans pseudorandom frequencies within the X-band at 45 Hz, electronically sweeping four directional bands simultaneously. The AESA radar can track 600 targets simultaneously including very high speed targets due to its high refresh rate; the radar can produce secondary target locks for the beyond-visual range Corseque Active Radar Homing missile through its entire range, or the missile can operate independently with the Headhunter's radar switched off. A Timing & Inertial Measurement Unit, or TIMU continuously self-calibrates the aircraft's location in relation to predetermined waypoints in the aircraft's mission plan, considered 99.85% accurate even in commuication or GPS-denied environments, the aircraft's computer provides turn-by-turn directions to the crew. If the aircraft is connected to the encrypted SANMEN communications network, mission parameters such as waypoints, targets, etc. can be changed in flight and updated to allow forces to rally or regroup instaneously.

Real World Comparison - - Dassault Mirage IV: PSI.43/2R4 is a fundamental ground-up rework of the Mirage IV concept, so they are extremely similar aircraft. Headhunter is half a meter longer than Mirage IV, with a wider wingspan and a greater wing area by eight square meters. Consequently, wing loading numbers are similar due to Blackheart's higher maximum takeoff weight. PSI.43's engines are much more modern and far more powerful than those carried by Mirage IV, so thrust to weight ratio is dramatically superior to the Mirage, as is the aircraft's maximum service ceiling and climb rate. Headhunter's internal fuel volume is significantly higher than Mirage IV due to the higher fuel consumption required by the MTV45.112R; combat range and ferry range for Mirage IV are broadly similar to rated endurances for Blackheart at supercruise and at its VNE, however Blackheart covers those distances at much greater speed. The greatest differences between the two aircraft lie in their avionics and in intended role; Blackheart's 2020 and 2022 modernizations saw all-glass cockpits and modern sensor suites integrated, where Mirage IV was being stood down by the mid-1970s. The Marquesan aircraft, while similar in shape and overall performance to Mirage IV, is employed for the deployment of primarily long-range precision guided glide bombs and heavy anti-shipping and radar homing missiles like Corseque and Sarissa, with secondary mission profiles for direct overflights of active combat zones.

Flyaway Cost Per Unit:(Place orders Here.)
183,000,000 NSD.

Research Links:
Last edited by Marquesan on Mon Nov 13, 2023 6:23 am, edited 35 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Civil Rights Lovefest

SSP.47/3R3 "Blackheart"

Postby Marquesan » Sat Sep 19, 2020 8:27 pm


Image
Artwork by Lauzanne.

Nomenclature: SSP.66/3R3 "Blackheart"
Classification:
Supersonic Strike/Penetrator

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service
January 1st, 1966

Program Cost:
2,040,000,000 NSD

Number Built:
340

Specifications:

Crew:
3 (Pilot, Co-Pilot, Weapons Officer)

Overall Length:
29.75 meters (96'9")

Tail Height:
6.20 meters (20'4")

Wingspan:
17.90 meters (58'9")

Wing Area:
165.33 m2 (1,780 ft2)

Wing Loading:
403.19 Kg/m2 @ MTOW (76.94 Lbs/ft2)

Empty Weight:
24,000 Kgs (52,911 Lbs)

Internal Fuel:
38,810 liters - 31,390 Kgs (69,203 Lbs)

Gross Weight:
55,390 Kgs (112,113.9 Lbs)

Payload Capacity:
Internal Ordinance - 11,270 Kgs (24,846 Lbs)

Max Takeoff Weight:
66,660 kgs (136,960 Lbs)

Powerplant:
2x HTV140.200R Thrust Vectoring Turbofans

Rated Thrust:
138.65 kN @ Military Power, 246.45 kN @ Reheat each

Thrust-to-Weight Ratio:
0.75:1 @ MTOW (kgf:kg)

Fuel Burn:
3.28 Kg/Sec @ Supercruise, 15.85 Kg/Sec @ VNE

Performance:

Supercruise Performance:
6,500 Km (4,038.91 miles) in 3 hours @ 2,126 Km/H (Mach 1.72)

Maximum Performance: (VNE - above 13,915 meters / 45,652')
2,700 Km (1,677.7 miles) in 44 minutes, 16 seconds @ 3,655 Km/H (Mach 2.96)

Service Ceiling & Climb Rate:
25,600 meters (84,858') in 150 Seconds @ 170 M/Sec (33,464 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aLF "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Description:

At 94 feet in length and 47.3 tons maximum takeoff weight, SSP.47 "Blackheart" is among the largest and heaviest carrier-launchable tactical bombers in service anywhere in the world. Blackheart is powered by a pair of mid-bypass turbofan engines buried in the fuselage, with over-the-wing S-shaped intake tracts which obscure the faces of the bypass fans from radar, and thermally-insulated exhaust tracts. The bomber carries fourteen tons of fuel aloft, and is rated to carry nearly 25,000 pounds of ordinance in its ten-meter long central weapons bay. A 150-meter wing area permits a very moderate wing loading number, and consequently, a very high natural ceiling at nearly 85,000 feet. At full reheat, (afterburner) Blackheart climbs at more than 33,000 feet per minute, reaching its service ceiling in just over two minutes. From high altitude, Blackheart is rated to either sprint at 2,700 kilometers per hour (Mach 2.18) for more than 900 miles, or can cruise for two hours and forty minutes at Mach 1.29 from the Military Power setting. The Supersonic Strike Penetrator role for which Blackheart was designed requires extended high-speed flight deep into defended enemy airspace, so the primary focus of the design was a blend of speed, agility and stealth. To that end, the titanium honeycomb internal frame of the SSP.47 is built up in layers of Carbon Fiber-reinforced polymer; this construction method produces tremendous airframe rigidity and dramatically decreases parts count over more conventional aluminum-skinned designs. The extended high-temperature conditions Blackheart sees in combat operations required advanced cooling solutions, so leading edges are cooled with thermoelectric cooling plates built into the aircraft's skin, and the aircraft's fuel is cycled throughout the airframe, acting as a cooling fluid. The airplane has a flattened appearance, with built-in angles that make the aircraft less susceptible to radar. The air intakes and exhausts are jagged to reduce their radar signature and placed on top of the aircraft to keep them out of sight to radars operating below the bomber. Many components of the type's powerful Netane Kinetics MTV45.112R mid-bypass turbine engines are coated in high temperature ceramic to reduce thermal transfer to the airframe. The engines, buried in tunnels at the rear of the airframe use serpentine ducts over the wings to obscure the engine's bypass fans from radar. Thrust tunnels aft of the turbofans are lined in heat-absorbent ceramic tiles to reduce the thermal signature of the aircraft. Engine exhaust flows through troughs at the rear of the aircraft, shielding the engines from upward-looking heat seeking missiles. Blackheart is a semi-lifting body design, with thin, low-aspect swept wings and highly-canted ruddervators rather than a vertical tail and horizontal stabilizers. The three-person cockpit allows the copilot and weapons officer to sit abreast of each other behind the pilot, sharing the workload and the cockpit displays in a crew escape module. Just aft of the cockpit is a cavernous, 10-meter long ventral weapons bay, with a 5-shot weapons carousel specially constructed to carry very large, heavy-class standoff missiles or a stunning variety of smaller munitions. Blackheart's most potent anti-shipping payload layout typically includes five (5) "Witiko" sea-skimming supersonic cruise missiles, with a range range of more than 700. This payload and the aircraft that carries it are optimized for passing through defended airspace to deliver ordinance deep into enemy territory, while evading, outrunning and defeating hostile defenses.

SSP.47 carries the 1,500 watt X-band "Altair" AESA radar in a radar-transparent aerodynamic nosecone; this modern radar takes advantage of the latest advances in compact solid-state power systems and EMP-hardened system-on-chip scaled supercomputing, producing a lightweight radar of great power and high sensitivity in a rugged, flyable configuration. Altair can mark targets of even very small radar cross sections at distances of up to 400 kilometers and can track 600 targets simultaneously. The radar scans four directional bands simultaneously at pseudorandom frequencies in the X-band at 45 Hz, this allows Altair to track even very high speed air targets effectively. The radar can also be used to create crisp, clear radar images of surface targets, even under atmospheric obscurants like dust, rain or oil smoke, as when providing confirmation of damage while the target is burning. In addition, the Aquila optronics suite provides an above-nose blister for a dual-band M/WIR sensor and 10-megapixel visible light sensor aligned together with a power telephoto zoom lens, allowing identification and discrimination of distant targets in conjunction with the Altair radar. In addition, a below-nose blister provides a full suite of laser systems including a laser spot receiver, coded designator and 3D laser scanner. A Timing & Inertial Measurement Unit, or TIMU continuously self-calibrates the aircraft's location in relation to predetermined waypoints in the aircraft's mission plan, considered 99.85% accurate even in commuication or GPS-denied environments, the aircraft's computer provides turn-by-turn directions to the crew. If the aircraft is connected to the encrypted SANMEN communications network, mission parameters such as waypoints, targets, etc. can be changed in flight and updated to allow forces to rally or regroup instaneously.

Real World Comparison - - Tupolev Tu-22M: Tu-22M is longer than SSP.47 by nearly 13.8 meters, with a spread wingspan significantly wider than Blackheart's modified delta wing and more wing area overall. Tu-22M is significantly taller and nearly triples SSP.47's maximum takeoff weight, with twice the wing loading weight of Blackheart, and a significantly lower thrust-to-weight ratio than the smaller Marquesan bomber. The two aircraft are in similar roles, with a mission profile revolving around launching long-range missiles into high value targets from a supersonic penetration bomber, optimized for high speed operations and relatively long ranges from their launching facilities. SSP.47 is a significantly smaller, lighter, more powerful and faster aircraft than Tu-22, with a dramatically higher service ceiling and climb rate, though Blackheart's engines are signifcantly less powerful than the Kuznetsov NK-25s powering Tu-22. With more modern, fuel-efficient engines and signifcantly less fuel, Blackheart's maximum range of 2,640 miles is comparable to the 4,200 mile maximum range of the Soviet bomber, SSP.47's top speed at 2,700 Km/H comparable to the 1,997 Km/H maximum speed of Tu-22M, however Blackheart is designed for supersonic operations throughout its entire mission profile, and its weapons carriage significantly different from the internal/external layout of Tu-22M, which prioritizes its variable-geometry wing over stealth, a greater priority in the later years during which SSP.47 was developed. Tu-22M being a much larger aircraft, it can carry a much larger bombload, however the standard payloads are similar, and the mission profile similar enough to make the two aircraft significantly comparable, despite obvious disparities.

Flyaway Cost Per Unit:(Place orders Here.)
218,000,000 NSD.

Research Links:
Last edited by Marquesan on Mon Nov 13, 2023 6:37 am, edited 52 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
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Founded: Oct 21, 2010
Civil Rights Lovefest

AHI.12/1R2 "Morrigan"

Postby Marquesan » Mon Sep 21, 2020 11:57 am


Image
Artwork by Lauzanne.

Nomenclature: AHI.12/1R2 "Morrigan"
Classification:
Agile Hunter/Interdictor

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
June 17th, 1956

Program Cost:
1,440,000,000 NSD

Number Built:
720

Specifications:

Crew:
1 (Pilot)

Overall Length:
16.70 meters (54'9.5")

Tail Height:
4.80 meters (15'8.9")

Wingspan:
15.80 meters (51'10")

Wing & Canard Area:
42.25 m2 (454.78 ft2)

Wing Loading:
292.78 Kg/m2 @ MTOW (59.96 Lbs/ft2)

Empty Weight:
4,200 Kgs (9,259.42 Lbs)

Internal Fuel:
8,626.7 liters - 7,030 Kgs (15,498.50 Lbs)

Gross Weight:
11,230 Kgs (24,757.91 Lbs)

Useful Payload:
1,140 Kgs (2,513.27 Lbs)

Max Takeoff Weight:
12,370 Kgs (27,271.18 Lbs)

Powerplant:
1x TSF.23/60 Open-Rotor Propfan

Rated Power:
6,000 kW @ Military Power (8,046.13 HP)

Power-to-Weight Ratio:
650.21 HP/Ton @ MTOW (0.48:1 kw/kg)

Fuel Burn:
0.42 Kg/Sec @ Cruise, 2.45 Kg/Sec @ VNE

Performance:

Cruising Performance:
3,350 Km (2,081.6 miles) in 4 Hours, 35 Minutes @ 730 Km/H (453.6 MPH)

Maximum Performance: (VNE - above 4,460 meters / 14,632')
760 Km (472.25 miles) in 48 Minutes @ 955 Km/H (593.4 MPH)

Service Ceiling & Climb Rate:
14,150 meters (46,423') in 4 Minutes, 27 Seconds @ 52.9 M/Sec (10,414 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLF "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 1x AC22.L82/2 Dual-barrel autocannon @ Lower Chin Mount w/ 1,050 Rds

Hardpoints: (6x; 3 per wing, semi-recessed)
- AGR.18HV "Stiletto" Laser-Guided 80mm Air-to-Ground Rockets (10-Round Pods)

- AGR.19ER "Kestros" Laser-Guided 140mm Air-to-Ground Rockets (5-Round Pods)

- MHL.201R2 "Fire Lance" Radar-Homing AAMs (6-Rd Pods)

- ATW.130R3 "Partizan" Wire-Guided Hypersonic ATGMs (4-Rd Boxes)

- TAT.105 "Cinquedea" Subsonic Thermal ATGMs (Double Pylons)

Description:

The proposition of developing a fixed-wing Close Air Support fighter in 2020 was carefully considered. In the current battlespace, there are many threats which did not exist 40 years ago or more, however there is a persistent need for aircraft to deliver ordinance precisely on ground targets despite the threat of ever-smaller Surface-to-Air missiles and the proliferation of Self-Propelled Anti Aircraft Guns. The FMA turned its eyes toward a radical design codenamed "Morrigan" placing a large, custom-developed 8,000 horsepower turbo-propfan at the rear of an aircraft with forward swept wings and nose-mounted canards. Giving 650 horsepower per ton, the open-rotor propfan is unusual but efficient, with two banks of counter-rotating "scimitar" blades driving the aircraft faster than nearly all propeller-driven aircraft in the world today. The airframe is extremely compact at 55 feet in overall length and 52 feet from wingtip to wingtip. The design makes use of modern compact avionics, saving space internally for a twin-barrel 22mm autocannon, its 71-inch barrel and dual 1,050-round magazine behind an armored cockpit, with the gun running beneath, and a low-RCS housing that conceals all but the muzzle, which is designed to deflect the blast of firing forward and not into the cockpit, which is sound and vibration deadened inside the titanium "bathtub" the pilot sits in. Three wing-mounted pylons on each wing carry a stunning array of powerful armaments; a typical loadout includes twelve (12) "Cinquedea" tandem-warhead ATGM's and eight hypersonic "Partizan" missiles on racks of three and four. Wingtip pods house duplicated Electro-Optical Targeting Systems, while the nose houses a modern, compact X-band AESA radar. This separated layout puts the greatest distance between the radar, the gun, the engine and the optical sensors, which minimizes distortion, increases accuracy and allows the nose of the aircraft to be simpler, monolithic, armored against 30mm cannonfire and made more aerodynamic.

Morrigan's forward-swept wings house the aircraft's fuel in flexible braided-Kevlar fuel cells which reduces the chance of catastrophic fuel loss in the event of taking fire. Morrigan's layout and light weight permit it extraordinarily-low wing loading in flight; the aircraft's stall speed is only 90 miles per hour, while maximum level flight speed is 515. Capable of extremely tight turns and sharp direction changes, Morrigan fighters are capable of maneuvering at speed through the tightest canyons, a skilled pilot can produce acrobatic maneuvers typically only seen in air shows. Additionally, its propfan engine is extraordinarily fuel efficient, allowing cruising at 320 miles per hour for 7.3 hours, or loitering at slow speeds for much longer. Morrigan's 38mm autocannon places the weight of its action and magazines on the aircraft's center of gravity and the length of the gun permits the muzzle to be forward of the cockpit. The gun is tremendously powerful and accurate, firing in 66 or 130-round bursts against moving targets at a maximum of 2,000 meters against moving targets, or against fixed point targets at 4,900 meters. Ammunition leaving the AC22 cannon is fired at a muzzle velocity of Mach 3.28 with 4:1 belts of thin-wall high explosive and armor-piercing ballistic cap rounds, producing kills on a wide variety of potential targets from other aircraft to tactical pillbox bunkers and armored vehicles. The heaviest targets can be prosecuted at nearly 30 kilometers distance with the TAT.105 "Cinquedea" ATGM. Cinquedea's top-attack methodology, 155mm diameter shaped charge primary and 7 kilogram Beryillium-enhanced HE tandem warhead combined with slightly supersonic flight speed and smokeless motor means it strikes without warning, diving on the target vertically from its design altitude of 100 meters. The weapon is Fire-And-Forget; it can be locked on by Morrigan's EOTS and once fired, uses its own high-definition L/WIR sensor to track the target, aiming for the hotspot above its engine. Closer in, targets can be attacked with the Partizan wire-guided missile. Carried in racks of four on Morrigan's outermost wing hardpoints, the Partizan missile is powered by an extremely high-impulse, short duration smokeless rocket engine which propels the wire-guided missile to Mach 6.5, reaching more than 11 kilometers in 5.5 seconds. The weapon is guided by a fiber optic filament from the launcher which disengages from the aircraft once the weapon is locked on its target and falls free. Partizan is both powerful and versatile; three types of payloads can be carried; Depleted Uranium long-rod penetrators, fuze-delayed anti-runway munitions, and an incendiary White Phosphorous/Magnesium round, intended to defeat lightly armored vehicle crews and infantry operating behind cover, as inside a building.

Real World Comparison - - LTV A-7 Corsair II: Morrigan is 2.7 meters longer than Corsair II, with 4.8 meter wider wingspan (due to Corsair's swept wing and Morrigan's forward-swept wing) and 7.42 square meters larger overall wing area. With 7 tons lower maximum takeoff weight and greater wing area, Morrigan benefits from enormously lower wing loading, with a higher ceiling despite being driven by an open-rotor propfan where Corsair II is turbofan powered. Morrigan's pusher-propfan arrangement with forward wing sweep and canards produces extremely tight turn and roll rates, with relaxed stability and fly-by-light fiber optic computer control far more sophisticated than Corsair II's avionics suite could have provided at the time of its production. Consequently, the extreme agility exhibited by Morrigan could not be matched by a turbine-powered, heavier, swept-wing aircraft. The two aircraft are assigned the same combat role as subsonic, naval close air support aircraft, making them eminently comparable, despite obvious differences in approach. Corsair II weighs twice the empty weight of Morrigan, and Morrigan carries aloft two and a half tons more fuel. Corsiar II carries a much heavier combat payload, in part due to Morrigan's reliance on guided missiles which are far more modern and much lighter than munitions Corsair II was certified to carry. Corsair II's maximum speed at 1,100 Km/H is only slightly higher than Morrigan's 955 Km/H Never-Exceed Speed (VNE) however the open rotor propfan is significantly louder than Corsair II's turbofan at that speed. Morrigan's engine is significantly more fuel-efficient, and with greater internal fuel load, can cruise much further than Corsair II at subsonic speeds. Morrigan's climb rate is inferior to Corsair II's by roughly 5,000 feet per minute, however its higher service ceiling and sharper low-altitude, slow speed handling are net advantages in the low altitude, close air support role these aircraft share. Corsair II carries a 20mm Vulcan rotary gun with 1,030 rounds vs. Morrigan's twin-barrel Gast-principle 22mm gun, with 1,050 rounds. The 22mm gun's limited burst fire modes allow the pilot to conserve ammunition while prosecuting targets with tight, measured bursts, where the Vulcan's higher rate of fire expends ammunition more quickly. In addition, the 22mm autocannon's ammunition is significantly lighter than the 20mm gun's, fired at a much higher muzzle velocity to a much higher maximum effective range, where Vulcan's effective range is roughly 600 meters, intended for much closer engagements. The 22mm gun, by contrast, is intended for engaging targets at much longer ranges, a theme common of the modern weapons carried by Morrigan such as Partizan hypersonic wire-guided missiles, Cinquedea subsonic anti-tank missiles and Bayonet thermal air-to-air missiles. Corsair II's armament by contrast is oriented toward guided gravity bombs and high-speed anti-radiation missiles and less toward prosecution of pinpoint battlefield targets.

Flyaway Cost Per Unit:(Place orders Here.)
106,000,000 NSD.

Research Links:
Last edited by Marquesan on Mon Nov 13, 2023 6:49 am, edited 51 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
Kraven Prevails!

User avatar
Marquesan
Minister
 
Posts: 2247
Founded: Oct 21, 2010
Civil Rights Lovefest

CIR.76/2R2 "Corax"

Postby Marquesan » Mon Sep 21, 2020 7:08 pm


Image
Artwork by New_Aeyariss.

Nomenclature: CIR.76/2R2 "Corax"
Classification:
Counter-Insurgency/Reconnaissance Helicopter

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
April 15th, 1984

Program Cost:
24,950,000,000 NSD

Number Built:
9,100

Specifications:

Crew:
2+6 (Pilot, Weapons Officer & 6x Soldiers)

Fuselage Length:
14.80 meters (48'7")

Fuselage Width:
2.00 meters (6'6")

Mast Height:
4.00 meters (13'1")

Stub Wingspan:
4.60 meters (15')

Empty Weight:
3,160 Kgs (6,966.6 Lbs)

Internal Fuel:
3,190.5 liters - 2,600 Kgs (5,732 Lbs)

Gross Weight:
5,760 Kgs (12698.6 Lbs)

Payload Capacity:
1,840 Kgs (4,056.5 Lbs)

Max Takeoff Weight:
7,600 Kgs (16,755.1 Lbs)

Powerplant:
1x TSF.18/34 Free Power Turboshaft

Rated Power:
3,300 kW (4,425.37 Horsepower)

Power-to-Weight Ratio:
582.28 HP/Ton @ MTOW (0.43:1 kw/kg)

Fuel Burn:
0.11 Kg/Sec @ Cruise, 0.44 Kg/Sec @ Maximum

Rotor Diameter:
2x 10.90 meters (35'9" - Coaxial)

Disc Area:
186.62 m2 (2,008.76 ft2)

Disc Loading:
40.72 Kg/m2 @ MTOW (8.34 Lbs/ft2)

Performance:

Cruising Performance:
1,750 Km (1,087.4 miles) in 6 Hours @ 290 Km/H (180.2 MPH)

Maximum Performance:
680 Km (422.5 miles) in 97 Minutes @ 420 Km/H (261 MPH)

Service Ceiling & Climb Rate:
6,330 meters (20,768') in 8 Minutes, 48 Seconds @ 12.00 M/Sec (2,362.2 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 1x AC22.L82/2 Dual-barrel autocannon @ Shrouded Chin Mount w/ 1,050 Rds

Hardpoints: (4x Stub Wing-Mounted Pylon Hardpoints)
- AGR.18HV "Stiletto" Laser-Guided 80mm Air-to-Ground Rockets (10-Round Pods)

- AGR.19ER "Kestros" Laser-Guided 140mm Air-to-Ground Rockets (5-Round Pods)

- MHL.201R2 "Fire Lance" Radar-Homing AAMs (6-Rd Pods)

- ATW.130R3 "Partizan" Wire-Guided Hypersonic ATGMs (4-Rd Boxes)

- TAT.105 "Cinquedea" Subsonic Thermal ATGMs (Double Pylons)

Description:

The CIR.76 "Corax" Helicopter is the genesis of a series of lightweight, coaxial-rotor reconnaissance helicopters developed by and for the Marquesan Armed Forces. Corax, like all of the latest generation of Marquesan-built combat aircraft, is built on a semi-monocoque titanium honeycomb frame, built up with layers of Carbon Fiber-Reinforced Polymer and reinforced in some areas with additional titanium armor. The stealthy, extensively-modeled shape of the Corax helicopter affords it considerable versatility for a helicopter in this weight class. Corax flies with a single turboshaft engine rated to 3,300 kilowatts. The free-power turbine is locked to the rotor mast, enabling a differential between engine speed and rotor speed which makes Corax easy and forgiving to fly. The coaxial rotors spin counter to each other, eliminating rotor torque and the need for a tailrotor. Corax uses a flattened, tapering tail with canted ruddervators instead of a traditional tail with vertical and horizontal stabilizers. Hot turbine exhaust is split between port and starboard exhaust ports which are washed by the rotors to quickly dissipate the thermal signature of the engine; this helps protect Corax from heat seeking missiles. Additionally, the skin of the Corax helicopter has thermoelectric cooling plates layered strategically throughout the aircraft. These cooling plates respond to sensors outside the aircraft and match the temperature of the terrain around the helicopter. This passive system of adaptive camouflage operates any time the helicopter is flying near ground level at low speeds or hovering without pilot input or adjustment. The flattened, low-RCS shape of the Corax helicopter allows it to penetrate air defenses at low level, all angles have been carefully considered and cockpit glass has been coated and treated to mitigate cockpit radar reflections; the lack of a tail rotor contributes to a greatly reduced acoustic signature for Corax as well. The crew area of the CIR.76 helicopter is proofed to its own weapons, armored to resist 22mm cannonfire with all doors sealed including the glass. Corax has a pair of long spar wings, with Electronic Countermeasures pods at the tips and four weapons pylons underneath. The Adaptive Jamming Suite, or AES.40 monitors electromagnetic radiation received by its transponders. Hostile sources of electromagnetic radiation such as an enemy radar or communications signal is decoded by the AES.40 suite and once the software "learns" the hostile frequency, it applies up to 40 dB + or - gain, which is designed to overload and overheat the hostile radar, forcing it to shut down. In addition to this, the APAx2.250R "Rigel" fixed-panel AESA radar processes vertical and horizontal sweeps of the X-band at pseudorandom frequencies, refreshing at a rate of 30 Hz. Providing up to 250 watts of power and an involuntary detection range of 60 kilometers, the Rigel radar can maintain up to 400 simultaneous high-speed airborne tracks, or can produce precise 3D SAR images of ground targets, even through poor atmospheric conditions like fog, rain, smoke and blowing dust. Mounted to the mast, the 70-degree field of view provided by the radar allows the Corax helicopter to surveil and identify air and ground targets at moderate distances with a very low probability of intercept while the physical bulk of the helicopter remains concealed. The Aquila upper cockpit-mounted Optronics pod provides high-definintion thermal optics with a 40x magnification power telephoto zoom lens. Integrating a comprehensive laser suite with a dual-band M/WIR sensor and visible light sensor together, the Aquila pod can identify and track targets in all day/night atmospheric conditions, which allows Corax helicopters to hunt in conditions that normally preclude helicopter missions. There are two ventral and two dorsal pods on the helicopter for the Mahui Layered Defenses Suite, which nests missile warning receivers with 10-kilowatt infrared lasers. These lasers can be aimed at a maneuvering hostile missile with a very high degree of accuracy; this laser defense suite is designed to overload and destroy the missile's sensors, forcing it to veer off course or self destruct at a range of 2,000 to 30 meters from the aircraft. Up to four such missiles can be engaged by the system at any one time, which contributes to a very low loss rate for the Corax helicopter in combat conditions.

The Corax helicopter carries six soldiers in addition to its crew in a versatile cargo area to the aft of the cockpit, over the wings. Corax has sliding doors over both wings, permitting quick ingress and egress. Corax carries a 22mm, 82-caliber Gast principle autocannon, with two barrels operating from the firing recoil of the opposite barrel. The gun is tucked into a shrouded, under-chin mount, with muzzle blast directed away from the cabin. The gun is fixed facing forward, allowing for an effective recoil carriage mount that minimizes the effect on the helicopter's flight from firing the main gun. 22mm autocannon rounds are fired in automatically-limited bursts of 66 or 130 rounds from 4:1 linked belts of high explosive and armor piercing ammunition. This combination is effective against moving targets at two kilometers distance, and against fixed point targets at 4.9 kilometers range, far exceeding the typical range of 20mm Vulcan guns while maintaining a comparable rate of fire, with significantly lighter service ammunition. Four stub wing-mounted pylons can carry a huge variety of potential ammunition, however common armaments are "Fire Lance" radar-homing AAM's for prosecuting other helicopters and low-flying aircraft, "Partizan" wire-guided hypersonic ATGM's and "Cinquedea" ATGM's. Fire Lance is a 41-pound, solid fueled weapon, flying at Mach 1.57 to a maximum range of 4.3 miles and can climb to 12,700 feet, homing on its target with inverse monopulse radar homing and attacking with a 75mm diameter shaped charge warhead. Each Partizan weighs 53.6 pounds at launch, and fires a very high-impulse solid rocket motor, accelerating to Mach 6.56 at 100 g per second, attacking moving targets at 6.3 kilometers and fixed targets at 11.3 kilometers with one of three potential warheads, though the most common is a kinetic, depleted uranium dart powerful enough to defeat more than 1.2 meters of steel armor, guided to its target by fiber optic filament and the helicopter's sensors, resulting in extremely high accuracy with the hypersonic weapon. TAT.105 Cinquedea is a 127.3 pound barely-supersonic weapon with an 18 mile effective range and a sensitive thermal sensor, aided by inertial guidance and mid-course data link. Cinquedea accelerates to just above the speed of sound, traveling in just over a minute to its maximum range, and striking top-down with a 155mm shaped charge warhead which penetrates nearly 1.2 meters of modern composite armor. These tough, agile helicopters are optimized for tactical insertion and penetration/interdiction missiles. A favorite of special operations personnel everywhere due to its very high degree of multi-spectrum low observability, high agility due to its high-horsepower turboshaft engine, light weight and very low disc loading, and high top speed due to coaxial rotors compensating for loss of lift on the retreating blade, the CIR.76 is a truly superior light attack helicopter for 21st century battlefields.

Real World Comparison - - Eurocopter Tiger: Real World Comparison - - Eurocopter "Tiger": Corax is slightly longer than Tiger, with a slightly higher mast due to its coaxial rotors, and 1.6 tons higher maximum takeoff weight. Two main rotors instead of one means Corax has a greater disc area despite having smaller overall rotor diameter; in addition to greater maneuverability due to lower disc loading, Corax can fly, hover and land in tighter spaces. Corax's single turboshaft engine is more powerful than the two smaller units on Tiger, affording a higher horsepower-per-ton, and a higher service ceiling with higher top speed. Maximum range for Corax is higher than Tiger due to carrying more fuel aloft, allowing for a 1,000+ mile cruising range and a 261 mile-per-hour top speed. Both helicopters have four external hardpoints for missiles and rockets, Tiger carries a single barrel 30mm gun with 450 rounds of ammunition in a chin turret, where Corax carries a twin-barrel 22mm autocannon fixed forward, giving an advantage to Tiger for not needing to turn the helicopter to engage a target. Finally, Tiger carries only its pilot and weapons systems officer, while the lack of a tail rotor or its machinery allows for a space in the rear of the Corax helicopter to transport six soldiers.

Flyaway Cost Per Unit:(Place orders Here.)
29,000,000 NSD.

Research Links:
Last edited by Marquesan on Wed Nov 15, 2023 4:02 am, edited 39 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Civil Rights Lovefest

HKA.12/2R3 "Hellcat"

Postby Marquesan » Sat Sep 26, 2020 8:48 am


Image
Image
Artwork by Aerospace Innovation Inc.

Nomenclature: HKA.12/2R3 "Hellcat"
Classification:
Hunter/Killer Assault Helicopter

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
October 3rd, 1980

Program Cost:
26,390,000,000 NSD

Number Built:
3,770

Specifications:

Crew:
2+10 (Pilot, Weapons Officer + 10x Soldiers)

Fuselage Length:
18.30 meters (60')

Fuselage Width:
2.50 meters (8'2")

Mast Height:
4.80 meters (15'9")

Stub Wingspan:
7.40 meters (24'3")

Empty Weight:
5,670 Kgs (12,500.2 Lbs)

Internal Fuel:
4,130.5 liters - 3,366 Kgs (7,420.7 Lbs)

Gross Weight:
9,036 Kgs (19,921 Lbs)

Payload Capacity:
2,714 Kgs (5,983.3 Lbs)

Max Takeoff Weight:
11,750 Kgs (25,904.3 Lbs)

Powerplant:
2x TSF.18/34 Free Power Turboshafts

Rated Power:
3,300 kW (4,425.37 Horsepower) each

Power-to-Weight Ratio:
753.25 HP/Ton @ MTOW (0.56:1 kw/kg)

Fuel Burn:
0.14 Kg/Sec @ Cruise, 0.52 Kg/Sec @ Maximum

Rotor Diameter:
2x 15.00 meters (49'2" - Coaxial)

Disc Area:
353.4 m2 (3,803.97 ft2)

Disc Loading:
33.25 Kg/m2 @ MTOW (6.80 Lbs/ft2)

Performance:

Cruising Performance:
1,930 Km (1,199.25 miles) in 6 Hours, 17 Minutes @ 307 Km/H (190.76 MPH)

Maximum Performance:
720 Km (447.38 miles) in 1 Hour, 48 Minutes @ 402 Km/H (249.79 MPH)

Service Ceiling & Climb Rate:
6,330 meters (20,768') in 7 Minutes, 30 Seconds @ 14.0 M/Sec (2,755.9 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 1x AC30.L58/2 Dual-barrel autocannon @ Shrouded Chin Mount w/ 958 Rds

Hardpoints: (10x Stub Wing-Mounted Pylon Hardpoints)
- AGR.18HV "Stiletto" Laser-Guided 80mm Air-to-Ground Rockets (10-Round Pods)

- AGR.19ER "Kestros" Laser-Guided 140mm Air-to-Ground Rockets (5-Round Pods)

- MHL.201R2 "Fire Lance" Radar-Homing AAMs (6-Rd Pods)

- ATW.130R3 "Partizan" Wire-Guided Hypersonic ATGMs (4-Rd Boxes)

- TAT.105 "Cinquedea" Subsonic Thermal ATGMs (Double Pylons)

Description:

The HKA.118 Helicopter, codenamed "Hellcat" during development is the genesis of a unique design requirement for a 12-ton assault helicopter, capable of carrying enough missiles and rockets to serve effectively in a heavy anti-tank role while transporting a squad of 10 soldiers into combat. This design requirement evolved into the Hunter/Killer, Assault helicopter. Hellcat is built on a titanium honeycomb core, built up with layers of woven titanium cloth and Carbon Fiber-Reinforced Polymer. The fuselage of HKA.118 is protected from 14.9mm and lesser caliber guns including rotary guns from all angles and all glass is rated for multiple hits from 10mm and lesser calibers. Radar cross-section of the helicopter has been minimized to a practical point; Hellcat has the RCS of a large eagle, rather than a helicopter. HKA.118 is built around its two large 3,300 kilowatt turboshaft engines, with shrouded intakes to lower the Radar Cross Section. The turbine exhausts are diffused and washed by the rotors, dramatically lowering Hellcat's thermal signature over comparable designs. Power is transmitted to the rotors via free power turbines, which allow a differential between engine speed and rotor speed and allow one engine to transmit power in the event of an engine failure. Hellcat's high thrust-to-weight ratio and very low disc loading are due to its powerful, compact advanced turbines and contrarotating coaxial rotor system. The coaxial rotor has several advantages over a single rotor arrangement for this role, permitting a much higher top speed due to compensation for loss of lift on the retreating rotor, does not require a tail rotor and is therefore mechanically simpler and more damage resistant, the powerplant weighs less than equivalent helicopters therefore allowing for greater payload and a spacious crew area, large enough to carry ten soldiers into combat. Large anhedral stub wings carry five weapons pylons on each; these carry a combination of up to 70 rockets or 40 multirole missiles at maximum, or as most often flown a combination of both.

Hellcat is a long range, high-speed troop transport optimized for low level penetration of hostile airspace and engaging ground forces in support of intensely opposed Air Assaults; it is armed with a 28.7mm high-velocity autocannon at the nose, which fires from a revolving six round ammunition cylinder and a linkless, automatic feed. The cannon may be operated either in Burst mode in which all six cylinders will be expended at a fast rate of fire, but then must reload all six cylinders affording a few seconds for barrel cooling, or in a slower continuous semi-automatic mode. The gun carries a 1,080 round helical drum magazine just aft of the cockpit and is slaved to the pilot's Helmet-Mounted Display. The gun is powerful, able to engage armor at ranges of 5-9 kilometers. The highly accurate weapon has a 2.1 meter barrel contributing to its uncommonly high muzzle velocity with the 28.7x121.4mm service ammunition. The gun may either be loaded with armor-piercing finned Discarding-Sabot rounds or with G7 profile High Explosive/Incendiary rounds depending on the mission profile. The stub wings carry a combination of three primary weapon types; radar guided missiles, wire-guided rockets and long-range heat seeking missiles. The inverse-monopulse Fire Lance missile uses the powerful X-band radar onboard the helicopter to detect its target; the stable long range target lock afforded by the radar far exceeds the range of the lightweight Fire Lance missile, allowing a squadron of helicopters to network with each other, when some ships in the flight can operate with radars switched off and allow a few helicopters flying higher with radars active to provide overwatch while the remainder of the flight hunts. The highly agile Fire Lance is carried in large 11-round pods by the Hellcat, allowing each to stack dozens of missiles onto a single airframe. Also carried are 7-round pods for the wire-guided Partizan rockets. Each Partizan has an 8,000 meter, hair-thin fiber-optic cable reel internally, allowing it to fly with computer guidance from the helicopter. Partizan rockets cannot be jammed; their high speed and heavy warhead make them extremely useful for destroying bunkers, runways, fuel tanks or other precision targets that may not give a heat signature or radar signature. Partizan rockets are more than adequate to engage light naval targets, many armored vehicles, and can be used to engage infantry or deliver a number of warhead packages including smoke/illumination rounds, high explosive/incendiary rounds using shock insensitive beryllium-enhanced CL-20/HMX and a thermobaric round for destruction of light buildings, depots and infantry. For engagement of the heaviest ground vehicles, naval vessels up to the size of the largest destroyers and light cruisers and the highest flying fastest air targets, Hellcat helicopters carry 4-missile box launchers for the Misericorde missile, typically at the tip hardpoints. The OGM.189R2 "Misericorde" missile is a beyond visual range, very high speed heat-seeking missile, with a cooled M/WIR dual-band gimballed seeker behind a sapphire glass dome providing ultra high resolution tracking in all atmospheric conditions. Misericorde's 120 kilometer range, Mach 4 pursuit speed and maneuvering at 80 g give the missile a massive "no escape zone" in which the missile can be fired at a target far outside visual range before locking on and taking target identification data and midcourse updates from the helicopter, which allows Misericorde to engage a huge variety of targets. Misericorde is unique in that it carries the TAPHEI warhead, a tandem array with a shaped charge primary capable of penetrating the thickest modern battle tank armor and a high explosive/incendiary secondary which detonates inside the target with devastating effect.

Hellcat is equipped with an extremely modern all glass cockpit, pilot and copilot's helmets use Helmet-Mounted AMOLED displays with eye movement and voice sensors and accelerometers on the helmet, used for target prioritizing, weapons selection and a wide variety of other tasks designed to reduce the human workload of flying the helicopter. HKA.118's human inputs and systems all operate on redundant fiber optic data transmission, with full computer control and automatic real-time optimization of flight control surfaces responding to pilot inputs. These "Human+" in flight correction systems make Hellcat extremely forgiving and simple to fly with Hands On Throttle And Stick (HOTAS) while the copilot is freed to concentrate on sensors, electronic warfare and communication systems. The APAx2.250F "Rigel" Radar benefits from the latest advances in compact solid-state power systems and EMP-hardened scaled supercomputing; it is one of the physically smallest radars in its power class, allowing tremendous versatility in its mounting, placed in the nose of the Hellcat helicopter. Its wide field of view is swept vertically and horizontally at 30 Hz, on pseudorandom frequencies in the X-band, making the radar extremely difficult to jam successfully and the probability of detecting the radar very low. The Rigel radar has a 60 kilometer involuntary detection and classification range for even very small RCS targets; it is capable of maintaining 400 simultaneous air tracks or producing incredibly clear and sharp SAR radar images of ground or naval targets even in very poor weather conditions. In combination with this, the Aquila Optronics pod provides a high definition all-weather sensor mounted to above the helicopter's cockpit. This allows the Hellcat to "peek" over trees and ridgelines while remaining largely hidden and hovering in relatively tight spaces like clearings or between buildings. A dual-band M/WIR sensor and 10-megapixel visible light camera are mounted behind a 40x power telephoto zoom lens on an ultra-smooth electrically driven gimbal that allows the ball to traverse independently of the helicopter and be returned to center quickly. Complete with a full package of lasers and lasor sensors, the Aquila pod is capable of marking targets for guided munitions. The all-weather sensor automatically corrects for poor atmospheric conditions such as dust, oil smoke and rain, which permits flying combat missions in instrument-only flying conditions for which helicopter flight is normally off-limits. HKA.118's resilient design is evident in every aspect of its construction, Hellcat was built for the rigors of "mudfighting" combat, low to the surface and slow, loitering over the battlespace and providing devastating attack capabilities far beyond that provided by most any other helicopter. The instantly-recognizable silhouette of the Hellcat Hunter/Killer Gunship is a feared symbol on the modern battlefield, epitomizing the close air support role for troops on the ground. The Mahui Layered Defenses Suite protects the helicopter from guided missiles with a distributed network of missile warning receivers and 10-kilowatt infrared lasers, which target, engage and destroy hostile incoming missiles by overheating their targeting systems, forcing the missile to either veer off course or self-destruct at ranges between 2,000 meters and 30 meters from the aircraft. On the Hellcat helicopter, Mahui can engage as many as 6 missiles simultaneously, with a response time of less than 500 microseconds.

Real World Comparison - - Mil Mi-24 "Hind": Hellcat is slightly shorter than Hind, in part due to lack of a tail rotor; Hind is taller despite Hellcat's coaxial rotors due to flatter, wider low-RCS shape. Hellcat is more than 2t lighter than Hind due to lightweight composite construction but has similar maximum takeoff weight. Hellcat's engines are 2x as powerful as Hind's, Hellcat has a dramatically higher top speed and half of Hind's disc loading due to coaxial rotor system, affording Hellcat far greater in-flight agility, superior rate of climb and ceiling and superior range due to much greater internal fuel load carried. Hind carries 8 soldiers, Hellcat carries 10 and significantly more armament on external stub-wing pylons. Hind's 12.7mm Yak-B cannon is inferior in all respects to the FA29.L74.R6 on Hellcat except for rate of fire, the 28.7mm cannon has a much lower rate of fire but greatly extended range and destructive power. Hind's 8 hardpoints vs Hellcat's 10 weapons pylons carry similar armament weights, but Hellcat's missiles and rockets are much more modern. Hellcat's broad multi-spectrum stealth including thermal signature management and RCS mitigation make it far less likely to be targeted successfully with heat-seeking or SARH/Active Radar Homing missiles, Hind's tail rotor and single disc arrangement creates much more noise than Hellcat's coaxial rotors, Hellcat is mechanically simpler with free power turboshaft engines rather than geared shafts. Hind's much older, significantly simpler avionics and sensor suite lacks much of the modern functionality of Hellcat's advanced electronics.

Flyaway Cost Per Unit:(Place orders Here.)
34,000,000 NSD.

Reference Material:
Last edited by Marquesan on Wed Nov 15, 2023 3:59 am, edited 39 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
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User avatar
Marquesan
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Posts: 2247
Founded: Oct 21, 2010
Civil Rights Lovefest

TTG.28/3R2 "Strider"

Postby Marquesan » Sat Sep 26, 2020 5:11 pm


Image

Nomenclature: TTG.28/3R2 "Strider"
Classification:
Tiltrotor Transport Gunship (STOVL)

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
August 23rd, 1978

Program Cost:
5,940,000,000 NSD

Number Built:
990

Specifications:

Crew:
3 (Pilot, Co-Pilot, Loadmaster)

Overall Length:
21.50 meters (70'6")

Airlift Capacity:
18 Stretchers / 38 Soldiers / 76 Evacuees

Tail Height:
5.70 meters (18'8")

Folded Wingspan:
16.90 meters (55'5")

Spread Wingspan:
26.20 meters (85'11")

Wing Area:
105 m2 (1,130.21 ft2)

Wing Loading:
270.47 Kg/m2 @ MTOW (55.4 Lbs/ft2)

Empty Weight:
7,830 Kgs (17,262.2 Lbs)

Internal Fuel:
13,694.8 liters - 11,160 Kgs (24,603.6 Lbs)

Gross Weight:
18,990 Kgs (41,865.8 Lbs)

Cargo / Sling Load Capacity:
9,590 Kgs (21,142.3)

Max Takeoff Weight:
28,400 Kgs (62,611.3 Lbs)

Powerplant:
2x TSF.45/112 Free Power Turboshafts

Rated Power:
9,720 kW (13,034.73 HP) each

Power-to-Weight Ratio:
917.93 HP/Ton @ MTOW (0.68:1 kw/kg)

Propellers:
2x 13.00 meter 4-Blade Pitch Adjustable (132.73 m2 Disc Area each)

Disc Loading @ Hover:
106.98 Kg/m2 @ MTOW (21.91 Lbs/ft2)

Fuel Burn:
0.51 Kg/Sec @ Cruise, 2.14 Kg/Sec @ VNE

Performance:

Takeoff & Landing Performance:
Takeoff in 850 meters (2,788') & 240 Km/H (149 MPH) / Vertical -or- Landing in 630 meters (2,066') @ 140 Km/H (87 MPH)

Cruising Performance:
2,770 Km (1,721.2 miles) in 6 Hours @ 460 Km/H (285.83 MPH)

Maximum Performance: (VNE - above 4,560 meters / 14,960')
1,220 Km in 1 Hour, 26 Minutes @ 844 Km/H (524.43 MPH)

Service Ceiling & Climb Rate:
12,450 meters (40,846') in 8 Minutes, 14 Seconds @ 25.2 M/Sec (4,960.6 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 2x AC30.L58/2 Dual-barrel autocannon @ Shrouded Chin Mount w/ 958 Rds each

Description:

The GSU.270 is a multimission, workhorse aircraft which is the standard medium-sized, long distance troop transport operated by the Marquesan Armed Forces and its allies. The Utility Gunship program stemmed from combat experience in the Sondrian theater where heavily-opposed airmobile landings resulted in many casualties. To soften the high loss rate, a large transport capable of carrying several mounted guns and airlifting light armored vehicles was designed. The final production aircraft is the GSU.270R2 "Strider" Gunship. Strider is a VTOL aircraft, built with ducted lift fans in its wings, driven by driveshafts from a pair of turboshaft engines. The lifting fans are covered by internal cowlings during horizontal flight, which are opened for vertical takeoff and landing. Like all other Marquesan aircraft, Strider is built on a honeycomb frame made from titanium, built up with layers of Carbon Fiber-Reinforced Polymer. This construction method dramatically decreases the parts count from previous metal-skinned versions of these aircraft, and also dramatically increases airframe rigidity. Strider's semi-lifting body design utilizes a wide, flattened oval mission area designed to transport 40 soldiers and all gear. The aircraft is built with an armored cargo/passenger area protected at all angles from 15mm gunfire and below including smaller caliber rotary guns. Cockpit glass is armored and coated to reduce radar reflections from the cockpit, and the aircraft's radar, infrared and acoustic signatures have been carefully considered during the design process. The GSU.270's engine intakes are serpentine ducts which obscure the bypass fan from radar; inlets are above the wings and behind the cockpit, to exclude gun gases from entering the inlet and to minimize the chance of foreign object damage during takeoff and landing. The widely spaced tail has canted vertical sections and wide but thin horizontal stabilizers. Downward winglets on the tail and upward winglets at the wingtips increase stability, which is under full-time computer control. The "best of both worlds" design achieves slow-speed performance and sling-load capability with two 6-ton hooks on the aircraft's belly eclipsed only by large, dedicated heavy lift helicopters; the initial Strider Utility Gunship type replaced several aircraft including a dedicated lift helicopter. As a troop transport, its advanced, lightweight design, large wing area and fuel-efficient turboshaft engines afford it excellent handling characteristics, a long transport range excellent resistance to combat damage while remaining flyable.

The GSU.270 program had naval use in the design from the outset, so Strider Gunships can be catapult-launched in case of less ideal takeoff conditions. The wings of the Strider Gunship can be folded for storage onboard a carrier, but when deployed its wide delta wing affords the GSU.270 low wing loading and forgiving, stable handling. The balanced thrust from its pair of coaxial contrarotating lift fans makes Strider an exceptionally stable hovering platform and when the driveshafts are disengaged from the free power turbines in horizontal flight, its low bypass turbofan engines provide adequate thrust to propel the aircraft to a maximum speed of Mach 0.86, making it considerably faster than all of the STOL turboprop aircraft in its class and all but a handful of the jet aircraft in its class. Though Strider can be used to insert paratroopers, its excellent hover performance and quiet lift fans make it an ideal craft for low level tactical insertion of troops. In defense of itself and the troops it deploys, Strider gunships are designed with a four-barrel gas-driven rotary cannon on a swiveling chin mount. The high velocity 28.7mm ammunition it fires packs sufficient punch to destroy tracked armor; the 2.1 meter long barrels rotate at 4,240 RPM, driven by the recoil energy of the first round fired, so the gun spins up to full rotation almost instantaneously. The gun is programmed with selectable 200 or 400 round bursts, slaved to the movements of the Weapons Officer's helmet. The gun tracks targets using the Aquila Electro-Optical targeting pod on the nose of the aircraft, forward of the cockpit. The fixed field of view of the forward-facing blister corresponds to the maximum angles permitted by the gun's flexible linkless feeder; within these limits, the gun is slaved to the Warfare Officer's helmet-mounted display. This versatile optronics pod contains a dual-band M/WIR sensor and 10 megapixel visible light CCD, mounted coaxially behind a 40x power telephoto zoom lens, which permits the sight to be zoomed optically to mark targets at greater distances. The all-weather, day/night sensor automatically compensates for changing light conditions and atmospheric obscurants such as fog, rain, blowing dust or oil smoke. The Strider gunship is thus permitted to fly in instrument-only conditions typically restricted for aircraft of this type, and to take off and land vertically during those missions. The APAx2.250F radar takes advantage of the latest compact solid-state power systems and EMP-hardened scalar supercomputing; it is one of the smallest radars in its class, mounted in the nose of the GSU.270. The "Rigel" radar is a highly advanced X-band AESA, scanning horizontally and vertically at 30 Hz along pseudorandom frequencies in the X band. The radar is extremely precise and has an involuntary detection range for even very small RCS targets of 60,000 meters, an extremely low probability of intercept due to its low power and randomized electrical scanning. The Rigel radar can follow 400 simultaneous high-speed air tracks, or produce stunningly clear SAR images of surface targets. The radar's inputs are coherently blended with inputs from other onboard sensors and presented to the crew on a wraparound multifunction "all glass" cockpit display. Sitting three abreast as in the Strider gunship, the crew shares the use of large-format AMOLED screens which present all necessary information during flight, moving maps with Blue Force Tracking, known threats and turn-by-turn directions provided through the SANMEN encrypted communications network. GSU.270 as all modern Marquesan aircraft operate on "fly-by-light" redundant fiberoptic cable, the advanced central computing network reduces the number of separate systems onboard the aircraft and increases the speed and clarity of decisionmaking for the aircraft's crew and produces heightened awareness of the battlespace. Computer control of all flight surfaces produces a tremendously neutral flight character, with movements of the control surfaces responding to sensor inputs and pilot commands.

Real World Comparison - - Bell-Boeing V-22 "Osprey": The Strider Gunship is considerably larger than the V-22 Osprey, 3 meters longer with nearly twice the unfolded wingspan and four times the wing area. Strider's maximum vertical takeoff weight and Osprey's maximum Short Takeoff weight are nearly identical, but Strider is actually 3t lighter empty than Osprey due to much lighter titanium/CFRP construction. Strider has twice the airlift capacity of V-22 and comparable combat/ferry ranges though Strider has longer range and more fuel-efficient engines, both subsonic aircraft but Strider has a higher straight-line speed where V-22 can land in more compact spaces/more aircraft can be stored in the same space required for a Strider gunship. V-22 carries smaller machine guns, Strider carries a single swiveling autocannon. Strider's ducted fans are much more efficient, quieter and smaller than the tiltrotor arrangement on V-22; GSU-270 is a generational leap from V-22 and outperforms it in most every metric in the same aircraft category.

Flyaway Cost Per Unit:(Place orders Here.)
85,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 7:13 am, edited 32 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Marquesan
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Civil Rights Lovefest

TTH.136/6R2 "Vulcan"

Postby Marquesan » Thu Oct 01, 2020 6:25 am


Image

Nomenclature: TTH.136/6R2 "Vulcan"
Classification:
Tiltrotor Transport, Heavy (STOVL)

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
March 1st, 2005

Program Cost:
35,000,000,000 NSD

Number Built:
2,500


Specifications:

Crew:
7 (Pilot, Co-Pilot, Engineer, Loadmaster + 3x Gunners)

Airlift Capacity:
72 Stretchers / 150 Soldiers / 300 Evacuees

Overall Length:
38.00 meters (124'8")

Tail Height:
13.50 meters (44'3")

Folded Wingspan:
26.50 meters (86'11")

Spread Wingspan:
41.20 meters (135'2")

Wing Area:
169.7 m2 (1,826.63 ft2)

Wing Loading:
803.18 Kg/m2 @ MTOW (164.5 Lbs/ft2)

Empty Weight:
62,800 Kgs (138,450.3 Lbs)

Internal Fuel:
45,097.1 liters - 36,750 Kgs (81,019.9 Lbs)

Gross Weight:
99,550 Kgs (219,470.2 Lbs)

Payload Capacity:
36,750 Kgs (81,019.9 Lbs)

Max Takeoff Weight:
136,300 Kgs (300,490 Lbs)

Powerplant:
4x TSF.45/112 Free Power Turboshafts

Rated Power:
9,720 kW (13,034.73 HP) each

Power-to-Weight Ratio:
382.53 HP/Ton @ MTOW (0.28:1 kw/kg)

Propellers:
2x 17.0 meter 4-Blade Pitch Adjustable (227 m2 Disc Area each)

Disc Loading @ Hover:
300.22 Kg/m2 @ MTOW (61.49 Lbs/ft2)

Fuel Burn:
0.91 Kg/Sec @ Cruise, 2.59 Kg/Sec @ VNE

Performance:

Takeoff & Landing Performance:
Takeoff in 1,070 meters, (3,510') Vertical -or- Landing in 1,385 meters (4,544') @ 110 Km/H (68.35 MPH)

Cruising Performance:
7,030 Km (4,368.2 miles) in 11 Hours, 10 Minutes @ 630 Km/H (391.46 MPH)

Maximum Performance: (VNE - above 5,000 meters / 16,404')
3,075 Km (1,910.7 miles) in 4 Hours @ 780 Km/H (484.67 MPH)

Service Ceiling & Climb Rate:
12,450 meters (40,846') in 8 Minutes, 14 Seconds @ 25.2 M/Sec (4,960.6 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Armaments:

Autocannon:
- 3x FA22.L82.C2R (@ Rear, Left & Right Doors - Manual Operation) each

Description:

The Tiltrotor Dropship program set out with the goal of creating a tactical airlifter that could travel with airmobile troops and bring tracked or wheeled armor directly to contested landing zones. The Dropship needed to be capable of long-distance hauling at subsonic speeds with efficient modern powerplants and needed outstanding, stable slow-speed hover. The result of that program's completion is the TAD.855 "Vulcan", now in its second revision. The Vulcan Dropship is a modern, low-observable shape made with an internal titanium "honeycomb" core, each part built up with layers of Carbon Fiber-Reinforced Polymer, or CFRP. Making use of titanium as a structural element and building the airplane out of layers of carbon fiber allows for extraordinary rigidity and a spacious interior cargo space, capable of transporting 120 soldiers and all their gear, or loading a variety of armored vehicles or equipment. The design includes low-RCS features like highly-canted ruddervators instead of a cruciform tail and extensive modeling to minimize the radar cross section, acoustic signature and thermal signature of the aircraft. The skin of the Vulcan airframe has electrothermal cooling plates built into the carbon fiber polymer layers; these electric plates actively cool the skin of the aircraft to dramatically reduce its thermal signature. This aids in the evasion of heat seeking missiles, which are also countered by the Mahui Layered Defenses System. Mahui LDS is a "soft kill" laser defense suite which uses a distributed network of missile warning receiver heads along the ventral and dorsal centerline of the aircraft. The receivers precisely target projectiles moving as fast as 5,000 meters per second and have a response time of less than 500 milliseconds. The system uses 10 kilowatt infrared lasers to burn and overload the seekers and warheads on hostile missiles in flight, causing them to either veer off course or self destruct. On the Vulcan dropship, there are 6 laser heads, so the system can engage as many as 6 missiles at once. The tremendous versatility of the Vulcan airframe makes it a staple of the naval arm of the Marquesan Armed Forces, which uses Vulcan as the primary Carrier Onboard Delivery and heavy lift aircraft of the surface fleet, in addition to providing over the horizon assault capabilities to amphibious landings.

The aircraft is 36 meters long and weighs roughly 85 tons at maximum load. Its high wing is heavily reinforced, and carries a massive tiltrotor engine pack on either side of the straight wing. Each powerpack nests a pair of powerful turboshaft engines, each producing nearly 10,000 kilowatts of power. The engines are Free Power Turbine designs, which gear a driveshaft to the output of a turbine wheel in the exhaust path of a jet turbofan engine. The turbine wheel spins freely of the rest of the engine and pushes a driveshaft which powers the lift fan at the front of the pod. In this arrangement, each engine spins a driveshaft, one inside the other, powering counter-rotating 13-meter propellers. This four-engine powerpack gives Vulcan tremendous lifting power; it is the largest such VTOL tiltrotor in service in Esvanovia and possibly the world. Vulcan's power and extended range make it a staple of heavy lift logistics units, but it is often called upon to fly into contested landing zones. To this end, the entire cargo area is armored to resist 23mm gunfire and below, and the Vulcan Assault Dropship is well-armed. There are two forward-facing four barrel 28.7mm cannons under the aircraft's nose. These cannon fire in selectable 200 or 400 round bursts; their 2.1 meter long barrels afford very high muzzle velocity and a flat-shooting ballistic trajectory out to a maximum range of more than 9 kilometers. Together, the two weapons are devastatingly powerful; an 800 round burst is typically enough to destroy a moderately sized concrete building completely, and such sprays are horrific if employed against troop concentrations. In addition, rear, port and starboard exit doors have swing-out weapons turrets for dual-barrel 14.9mm machine guns. Using beltless electric feeds and two barrels to effectively double the rate of fire by using the energy of firing one to load the other, these "Gast Principle" guns are accurate out to nearly 6 kilometers and have a steady 660 RPM rate of fire which is adequately air cooled when fired with the barrels outside the aircraft, for indefinite belts of fire. The guns are remotely aimed by the computer and fully controlled by the weapons officer, using full color "false daylight" thermal optics to discriminate targets from friendly forces.

Real World Comparison - - Lockheed AC-130A "Spectre": Vulcan is longer than AC-130A by roughly six meters and slightly taller. Wingspan is nearly identical, but Vulcan can fold its wings for stowage aboard a carrier. Vulcan has a higher maximum takeoff weight by roughly 15 tons; this is in part due to the stronger titanium honeycomb construction and partly due to large difference in horsepower to weight ratio. AC-130A's wing area is slightly larger and has lower wing loading than Vulcan, but Vulcan is tiltrotor and can take off, hover and land at zero airspeed. AC-130A has a higher maximum ceiling by roughly 1,000 meters but has a shorter maximum range due to the greater fuel-efficiency of the more modern turboshaft engines on Vulcan. Vulcan has two 28.7mm rotary guns and three 14.7mm guns, Spectre gunship has four 7.62mm miniguns and four 20mm miniguns; these are roughly similar but in both cases the Marquesan weapons have better ranges and lower actual rates of fire with higher velocity, heavier ammunition.

Flyaway Cost Per Unit:(Place orders Here.)
135,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 7:20 am, edited 18 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
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Founded: Oct 21, 2010
Civil Rights Lovefest

COD.45/2 "Khonsu"

Postby Marquesan » Wed Oct 07, 2020 1:16 pm


Image

Nomenclature: COD.45/2 "Khonsu"
Classification:
Command, Observation & Delivery Aircraft

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
July 30th, 1990

Program Cost:
34,850,000,000 NSD

Number Produced:
640

Specifications:

Crew:
2 + 20 (Pilot, Co-Pilot & 20x Passengers)

Overall Length:
32.00 meters (105')

Tail Height:
7.80 meters (25'8")

Folded Wingspan:
17.50 meters (57'5")

Spread Wingspan:
31.66 meters (103'10")

Wing Area:
109.02 m2 (1,173.48 ft2)

Wing Loading:
421.48 Kg/m2 @ MTOW (93.84 Lbs/ft2)

Empty Weight:
22,630 Kgs (49,890.6 Lbs)

Internal Fuel:
17,646.2 liters - 14,380 Kgs (31,702.5 Lbs)

Gross Weight:
37,010 Kgs (81,593 Lbs)

Payload Capacity:
8,940 Kgs (19,709 Lbs)

Max Takeoff Weight:
45,950 Kgs (110,120.9 Lbs)

Powerplant:
4x MTE47.94 Compact Mid-Bypass Turbofans

Rated Thrust:
32.3 kN @ Military Power each

Thrust-to-Weight Ratio:
0.28:1 @ MTOW (kgf/kg)

Fuel Burn:
0.25 Kg/Sec @ Cruise, 0.37 Kg/Sec @ Maximum

Performance:

Takeoff & Landing Performance:
Takeoff in 1,700 meters, (5,577') Landing in 655 meters (2,149')

Cruising Performance:
14,140 Km (8,786 miles) in 15 Hours, 50 Minutes @ 890 Km/H (553 MPH)

Maximum Performance:
10,480 Km (6,512 miles) in 10 Hours, 40 Minutes @ 980 Km/H (609 MPH)

Service Ceiling & Climb Rate:
15,770 meters (51,739') in 12 Minutes, 20 Seconds @ 21.3 M/Sec (4,192.9 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit

APAx2.250F "Rigel"
Classification:
Air/Ground 3D Targeting Radar, 2-Beam Processing, 70° FFOV

Operation Mode:
X-Band AESA, 250W ERP, 30 Hz Update Speed

Design Spec:
60,000 Meters Detection Range, 400 Simultaneous Tracks

Notes:
Lightweight/Compact, High Clutter Suppression, Fixed Panel

AMPI.aF "Aquila"
Airborne Stare & Scan System (EOSS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

Description:

The "Khonsu" program is named for the Kylarnatian aspect of the Moon. It is the result of a design specification for an executive transport, however its versatility has seen it produced in several variants. The airframe can take off in under 1,900 meters at just under 45 tons; it is capable of 12,000+ kilometer intercontinental range at a high cruising altitude of 15,000 meters and 900 Km/H. Khonsu is unique for using four small mid-bypass turbofans instead of two or three larger turbines. The aircraft's low-slung wing and four podded engines allow the lightweight pods to be changed quickly for repair; the long, tapered wing with winglets allows for excellent maneuverability and a large internal fuel load. The aircraft's engines, designed for the much smaller "Kharon" high altitude observation drone are extremely quiet and fuel-efficient. Their comparitively low temperature combustor and high air-mass flow produce a minimal infrared and acoustic signature and allow the aircraft to cruise at low throttle position, allowing a conservative fuel burn and a quiet cabin. Internally, the Khonsu aircraft can be configured to carry cargo, fuel or can be configured with 20 swiveling command chairs and computer work-stations. The Khonsu airframe is a thoroughly modern design, with a titanium honeycomb internal frame built up with layers of Carbon Fiber Reinforced Polymer, as all Marquesan combat aircraft are. This military-oriented construction permits high airframe rigidity and light weight while dramatically reducing parts count over a conventional metal aircraft. As an executive transport, the COD.45 "Khonsu" is fitted with additional sound deadening and seats 20 in very comfortable accomodations. Eight windows allow light into the cabin, which is dominated by computer workstations and swiveling chairs in a staggered side-by-side arrangement. Configured as a tanker, the seats and workstations are replaced with tanks for additional fuel and the bulk fuel distribution boom at the rear of the aircraft, with a dedicated boom operator monitoring high definition cameras. In a cargo configuration, Khonsu can carry more than 6 tons of supplies and equipment, making it a highly versatile, multi-mission aircraft which is operated as a civilian craft by Crown Marquesas Airlines and others and as a military aircraft by the Marquesan Armed Forces and its allies.

The COD.45 class is protected by the Mahui Layered Defenses Suite, which places laser warning receivers and 10-kilowatt infrared lasers in pods on the aircraft's ventral and dorsal centerline. Small and minimally-intrusive into the airstream, the sapphire crystal domed pods monitor the airspace for hostile oncoming projectiles, moving at up to 5,000 M/Sec. The system has a sub-500 millisecond response time, and effectively engages hostile missiles at ranges of 2,000 meters to 10 meters by overheating the missile's seeker and forcing it to power down, veer off course or self destruct. With six sensor/laser heads, Mahui can defend against six threats simultaneously. The aircraft's nose integrates an APAx2.250F "Rigel" X-Band Radar, which scans pseudorandom frequencies in the X-band on vertical and horizontal bands simultaneously at 30 Hz. This 250 watt, ultra-compact radar provides all-weather ground observation and object identification, or can track 400 simultaneous air tracks with a small-RCS involuntary detection and identification range of 60 kilometers. In addition, an Aquila compact optronics pod is placed forward of the cockpit on the nose, colocating a dual-band M/WIR sensor and a 10 megapixel visible light camera behind a 40x telephoto power zoom lens, allowing all-weather, day/night flight in instrument only flying conditions; the Aquila optronics blister automatically corrects for atmospheric obscurants and changing light levels to provide a crystal clear picture of what is ahead of the aircraft to the pilots. COD.45's can be launched and arrested on the decks of carriers, once empty of fuel, the wings can be folded for stowage. If operating from land-based airfields, they can land in as little as 730 meters and can operate from austere paved runways and tarmacs.

Real World Comparison - - Gulfstream G550:Nearly identical length and height, Khonsu has a wider wingspan. Khonsu has a higher maximum takeoff weight and is slightly heavier empty; 4x smaller 30 kN class turbofans vs 2x 60 kN class turbofans, in practical terms this is a very even tradeoff between the smaller quieter Khonsu engines and the larger engines on G550. Similar passenger loads but G550 carries less fuel and has similar range. Service ceiling is functionally identical, Khonsu has a slightly longer takeoff run but shorter landing run. Khonsu's four engines are designed for quick-replacement and ease of maintenance where G550 requires more substantial downtime for engine changes. Khonsu's wings fold for stowage on a carrier and its reinforced landing gear are designed for carrier launch, where G550 can only operate from civilian airfields.

Flyaway Cost Per Unit:(Place orders Here.)
70,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 7:25 am, edited 19 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
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Civil Rights Lovefest

RST.371/6R2 "Derecho"

Postby Marquesan » Thu Oct 08, 2020 12:13 pm


Image

Nomenclature: RST.371/6R2 "Derecho"
Classification:
Rapid Strategic Transporter

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
January 1st, 1967

Program Cost:
100,000,000,000 NSD

Number Built:
510

Specifications:

Crew:
6 (Pilot, Co-Pilot, Radar Officer, Radio Officer & 2x Loadmasters)

Airlift Capacity:
78 Soldiers on Sidewall Seats + 28x 7.75 m2 Pallets / 2x Chimera Mk. V MBT's

Overall Length:
60.00 meters (196'10")

Tail Height:
14.10 meters (46'3")

Wingspan:
68.5 meters (224'9")

Wing Area:
604 m2 (6,501.4 ft2)

Wing Loading:
614.23 Kg/m2 @ MTOW (125.81 Lbs/ft2)

Empty Weight:
95,360 Kgs (210,232.8 Lbs)

Internal Fuel:
130,554.5 liters - 106,390 Kgs (234,549.8 Lbs)

Gross Weight:
201,750 Kgs (444,782.6 Lbs)

Payload Capacity:
169,250 Kgs (373,132.4 Lbs)

Max Takeoff Weight:
371,000 Kgs (817,995 Lbs)

Powerplant:
2x HPT80.1370 High-Bypass Turbofans

Rated Thrust:
378.25 kN @ Military Power each

Thrust-to-Weight Ratio:
0.20:1 @ MTOW (kgf/kg)

Fuel Burn:
1.90 Kg/Sec @ Cruise, 5.15 Kg/Sec @ VNE

Performance:

Takeoff & Landing Performance:
Takeoff in 1,870 meters, (6,135') Landing in 860 meters (2,821') @ 245 Km/H (152.23 MPH)

Cruising Performance:
12,510 Km (7,773.35 miles) in 15 Hours, 30 Minutes @ 806 Km/H (500.82 MPH)

Maximum Performance: (VNE - above 5,000 meters / 16,404')
5,200 Km (3,231.13 miles) in 5 Hours, 45 Minutes @ 906 Km/H (562.96 MPH)

Service Ceiling & Climb Rate:
13,330 meters (43,733') in 18 Minutes, 20 Seconds @ 12.1 M/Sec (2,382 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit


APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aF "Aquila"
Airborne Stare & Scan System (EOSS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

Description:

The RST.260 "Derecho" is classified as a Rapid Strategic Transporter; the aircraft is capable of lifting 280 troops or more than 52,000 kilograms of vehicles, aircraft, small vessels, shipping containers, palletized loads or anything else. The aircraft is of a semi-lifting body design, with large blended wings which produces a wide, highly-usable cargo space on the interior of the aircraft, sufficient to accommodate even 40-ton tracked Infantry Fighting Vehicles. Derecho's long-haul capability with nearly 12,000 kilometers point-to-point range affords truly intercontinental range for military airlift. Derecho uses a pair of large high-bypass turbofan engines developed specifically for this aircraft generating nearly 380 kilonewtons of thrust at Military Power. The engines are at the rear of the aircraft, above the wings which masks their infrared signature from upward-looking surface to air missiles. The wide semi-lifting body design uses fly-by-light fiber optic cable to actuate all flight surfaces and full computer control gives the otherwise very large aircraft a forgiving feel to the pilot. A large, vertical T-tail, atypical of Marquesan aircraft for its higher radar cross section permits excellent control at high angles of attack, as when taking off. Because Derecho's engines are above the wings, they are highly resistant to intake of foreign objects or dust, and are cleared for use on austere or unimproved dirt roads and runways. Its crew of five share a wide all-glass multifunction display which wraps around the cockpit providing moving maps and interactive, touch-sensitive controls. The sophisticated Testudo Mk. IV Combat Management System combines the inputs of the onboard Kanaloa TIMU with updates provided over the encrypted broadband SANMEN network; this creates a "moving map" display for navigation that shows the locations of friendly forces, the suspected and reported locations of hostile forces and information about disposition and capabilities wherever available. Mounted in the nose, a 1,500-watt "Altair" X-Band radar and the Aquila Optronics blister identify, track, classify and monitor hundreds of simultaneous airborne targets in all weather conditions, the two systems working together to compensate for changes in light level and poor atmospheric conditions over thousands of square kilometers. Derecho is defended from heat seeking and radar-guided air-to-air and surface-to-air missiles by the "Mahui" Layered Defenses Suite. Mahui nests 12 missile warning receivers with 10-kilowatt Infrared Lasers along the dorsal and ventral spine of the aircraft. Covered by a sapphire dome which protrudes only slightly into the airstream, each missile warning receiver tracks fast-moving projectiles up to 5 Km/Sec with a response time of less than 500 milliseconds. Mahui engages targets at distances from 2,000 meters to 10 meters from the aircraft with a laser which overheats the missile's guidance systems and forces it to either veer off course or self-destruct.

RSTAT.371, Aerial Tanker:
The Aerial Tanker variant Derecho carries aloft an additional 70,000 liters of aviation fuel along with the necessary distribution systems and two flying booms operated by an additional crewmember by high-resolution cameras displayed on large screens in the crew area. The flying booms are simultaneously operable; a computer control system automatically balances fuel from the aerial refueling tanks and the Derecho's own fuel tanks to maintain aircraft stability.

RSTEW.371, Electronic Warfare:
The Electronic Warfare variant Derecho mounts a pair of side-looking synthetic aperture APAMR.600 "Deneb" ultra-wideband synthetic aperture imaging radars along the fuselage of the aircraft. Information from these two systems is fused together with the aircraft's own APAMR.300 data and information received from the field. Additional high-gain plasma antennae are housed on the RSTEW aircraft, along with an expansion of the Testudo Rosso suite aboard. A pair of Theia Prime Electro-Optical turrets are mounted on either side of the fuselage behind the crew area, allowing the Derecho to detect and directly image aerial or surface targets with extreme resolution and accuracy. The RSTEW aircraft also mounts a Magnetic Analomy Detector (MAD) array on a tail-sting extending behind the aircraft. An additional pair of APAMR.75 "Rigel" radars are mounted to the Derecho's wingtips, giving the aircraft unparalleled electronic warfare capabilities. Extremely accurate three-dimensional maps may be compiled by the RSTEW aircraft as it flies, simultaneously analyzing and prioritizing data for tactical use by other command chains. Because of the aircraft's very long range and high fuel capacity, the RSTEW Derecho may remain airborne for extended periods of time or can patrol thousands of kilometers in a single sortie.

Real World Comparison - - Lockheed C-141 "Starlifter": Starlifter is roughly 3 meters longer than Derecho, but with slightly smaller wingspan and less wing area due to Derecho's blended wing extensions. Starlifter is lighter empty by 30t but Derecho's maximum takeoff weight is 120t heavier. Derecho's dramatically more powerful engines give it a higher thrust-to-weight ratio than Starlifter at maximum takeoff weight; engines are also more fuel efficient and Derecho's higher fuel load gives it nearly twice the range of Starlifter. Derecho carries 100 more troops in its wider cargo area than Starlifter, 3,000 meters higher maximum service altitude and similar speeds, but Derecho needs to refuel less often, leading to simplified logistics vs. Starlifters.

Flyaway Cost Per Unit:(Place orders Here.)
145,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 7:29 am, edited 16 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Marquesan
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Civil Rights Lovefest

TER.381 "Orisha"

Postby Marquesan » Wed Oct 14, 2020 12:43 pm


Image

Nomenclature: TER.381 "Orisha"
Classification:
Rapid Executive Transport (Transport Exécutif Rapide)

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
June 15th, 1985

Program Cost:
34,080,000,000 NSD

Number Built:
1,420


Specifications:

Crew:
16 (Pilot, Co-Pilot, Radio Officer, Engineer & 12x Flight Attendants)

Passenger Capacity:
480 (Nominal, One-Class w/ multiple configurations available)

Fuselage Length:
73.30 meters (240'6")

Fuselage Diameter:
6.50 meters (21'4")

Tail Height:
19.30 meters (63'4")

Cabin Length:
55.70 meters (182'9")

Cabin Width:
5.80 meters (19')

Cabin Height:
5.80 meters (19')

Passenger Seating:
2 Decks, 240x 762mm (30") seats each

Floorplan:
2+2+2, 40 Rows + Lounges, Lavatories & Crew Spaces

Cargo Capacity:
26x 7.75 m2 pallets

Cargo Volume:
206.25 m3 (7,283.65 ft3)

Folded Wingspan:
53.00 meters (173'11")

Spread Wingspan:
74.90 meters (245'9")

Wing Area:
632.78 m2 (6,811.2 ft2)

Wing Loading:
601.94 Kg/m2 @ MTOW (123.28 Lbs/ft2)

Empty Weight:
127,000 Kgs (279,987 Lbs)

Internal Fuel:
206,587.3 liters - 168,350 Kgs (371,148.2 Lbs)

Gross Weight:
295,350 Kgs (651,532.1 Lbs)

Payload Capacity:
85,550 Kgs (188,605.5 Lbs)

Max Takeoff Weight:
380,900 Kgs (839,740.8 Lbs)

Powerplant:
4x HPT80.1370 High-Bypass Turbofans

Rated Thrust:
378.25 kN @ Military Power each

Thrust-to-Weight Ratio:
0.40:1 @ MTOW (kgf/kg)

Fuel Burn:
2.62 Kg/Sec @ Cruise, 4.50 Kg/Sec @ Maximum

Performance:

Takeoff & Landing Performance:
Takeoff in 2,630 meters, (8,628') Landing in 1,590 meters (5,216') @ 256 Km/H (159 MPH)

Cruising Performance:
15,875 Km (9,864.26 miles) in 17 Hours, 50 Minutes @ 890 Km/H (553 MPH)

Maximum Performance:
9,760 Km (6,064.58 miles) in 10 Hours, 20 Minutes @ 940 Km/H (584 MPH)

Service Ceiling & Climb Rate:
13,330 meters (43,733') in 18 Minutes, 20 Seconds @ 12.1 M/Sec (2,382 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact Unit


APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aF "Aquila"
Airborne Stare & Scan System (EOSS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Forward of Cockpit

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Fixed Blister, Forward Facing

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

Description:

Pending written description.

Flyaway Cost Per Unit:(Place orders Here.)
TBD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 7:37 am, edited 12 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Civil Rights Lovefest

PFC.R27R2 "Kharon"

Postby Marquesan » Wed Oct 14, 2020 2:46 pm


Image

Nomenclature: PFC.R27R2 "Kharon"
Classification:
Pathfinder/Forward Controller Drone

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
June 22nd, 1977

Program Cost:
4,920,000,000 NSD

Number Built:
1,230

Specifications:

Overall Length:
8.40 meters (27'6.7")

Tail Height:
1.45 meters (4'9")

Wingspan:
8.10 meters (26'6.9")

Wing Area:
10.75 m2 (115.71 ft2)

Wing Loading:
249.30 Kg/m2 @ MTOW (51.06 Lbs/ft2)

Empty Weight:
1,150 Kgs (2,535.3 Lbs)

Internal Fuel:
1,018.5 liters - 830 Kgs (1,829.8 Lbs)

Gross Weight:
1,980 Kgs (4,365.1 Lbs)

Payload Capacity:
700 Kgs (1,543.2 Lbs)

Launch Weight:
2,680 Kgs (5,908.4 Lbs)

Powerplant:
1x MTE47.94 Compact Mid-Bypass Turbofan

Rated Thrust:
32.3 kN @ Military Power

Thrust-to-Weight Ratio:
1.22:1 @ MTOW (kgf/kg)

Fuel Burn:
0.03 Kg/Sec @ Cruise, 0.18 Kg/Sec @ Maximum

Performance:

Cruising Performance:
4,410 Km (2,740.25 miles) in 7 Hours @ 625 Km/H (388.3 MPH)

Maximum Performance:
1,200 Km (745.6 miles) in 1 Hour, 15 Minutes @ 950 Km/H (590.3 MPH)

Service Ceiling & Climb Rate:
19,350 meters (63,484') in 4 Minutes @ 80 M/Sec (15,748 feet per minute)

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact AESA

APAx.10F "Deneb"
Classification:
Synthetic Aperture Imaging Radar

Operation Mode:
X-Band, 10W ERP, 20 Hz Update Speed

Design Spec:
10,000 Meters Imaging Range, 0.5 Meter Resolution @ 10 Km Altitude

Notes:
Ultralight Fire Control Radar, 55° Fixed Field of View

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Description:

The "Kharon" Pathfinder drone is a compact, supersonic observation drone intended to be flown into extremely hostile areas before an attack to mark the locations of threats and targets. While unarmed, the extremely stealthy drone carries the APAx.10F "Deneb" fixed-mounted AESA radar in its nose. The Deneb radar benefits from the latest advances in solid-state power systems and EMP-hardened scalar supercomputing; it is one of the physically smallest radars in its class produces stunningly clear SAR images of ground targets at 20 Hz. A rotating Aquila Optronics Pod is mounted in the lower nose of the PFC.R49, which colocates a dual-band M/WIR sensor with a 10 megapixel visible light camera, aligned together on a 40x telephoto power zoom lens. These sensors work together to automatically correct for all light conditions and atmospheric obscurants such as dust, fog, rain or oil smoke. The all-weather, day/night optronics system and X-band radar together produce extremely clear, fused broadband images of targets on the ground and provides extremely reliable identification of ground targets while having an extremely low probability of detection or jamming. Kharon drones have a full suite of battlefield lasers and laser receivers which allow the drone to mark targets for laser-guided munitions, designed to interface with the Varuna rocket in specific to destroy disguised targets on the ground, even in the presence of thermal camouflage. Inertial guidance is provided by the "Kanaloa" Timing & Inertial Measurement unit, a GPS-independent guidance system which delivers the drone from waypoint to waypoint without requiring a satellite uplink with pinpoint accuracy. The drone's onboard System-On-Chip "SparkRED" computer places 64 cores and two terabytes of onboard memory on a single chip housed in the TIMU. The high autonomy permitted by the system allows the pathfinder drone to continue its mission even in fully communications-denied environments, relaying information back once out of jamming range. The PFC.R49 drone is built on a titanium honeycomb frame, built up with layers of Carbon Fiber Reinforced-Polymer; this construction method permits an extremely stealthy shape with a very low parts count and precise, blended lines contributing to low observability. The small, mid-bypass turbofan engine developed from business jet turbines has a dorsal intake with a serpentine duct that obscures the bypass fan from radar. The engine's high pressure design blends jet exhaust with the ambient air in a trough behind the jet nozzle lined with heat-absorbent tiles, dramatically decreasing the drone's thermal signature to seekers below the drone. Kharon class drones can fly in terrain-following profiles or can follow high altitude waypoints or any combination dependent on the mission profile. The class is rated with a 2,000+ kilometer combat radius and is capable of supercruising just above the speed of sound in high altitude flight near its service ceiling. As a pathfinder drone, it is capable of marking hundreds of targets during its flight time and relaying that information back to the launching platform. In a loitering flight plan, the PFC.R49 drone uses its three 1,550nm battlefield lasers to mark targets for incoming munitions such as rocket artillery or subsonic cruise missiles, dramatically improving the accuracy of those weapons when a Kharon drone is loitering in the area. The drones are launched from an electromagnetic catapult with a 10 meter Linear Induction Motor. These catapults, much smaller than those on larger Fleet Aircraft Carriers are mounted to "Galeru" GMC.176 class Guided Missile Cruisers in pairs to allow for simultaneous launch; the drones land on shortened runways with arrestor cables on either side of the vessel's Hot Canister Launch cells.

Flyaway Cost Per Unit:(Place orders Here.)
35,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 8:08 am, edited 11 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Civil Rights Lovefest

SLM.R44(N) / SRD.R44 - "Meduza"

Postby Marquesan » Sat Oct 24, 2020 1:18 pm


Image

Nomenclature: SLM.R44(N) / SRD.R44 - "Meduza"
Classification:
Supersonic Loitering Munition / Reconnaissance Drone

Nation of Origin:
The Marquesan Union, Esvanovia

Date in Service:
April 10th, 1965

Program Cost:
634,800,000 NSD

Number Built:
920

Specifications:

Overall Length:
12.80 meters (42')

Overall Height:
2.25 meters (7'4.5")

Wingspan:
6.64 meters (21'9.4")

Wing Area:
24.75 m2 (266.4 ft2)

Wing Loading:
178.98 Kg/m2 (36.66 Lbs/ft2)

Empty Weight:
1,230 Kgs (2,711.7 Lbs)

Internal Fuel:
3,558.7 liters - 2,900 Kgs (6,393.4 Lbs)

Gross Weight:
1,980 Kgs (4,365.1 Lbs)

Warhead Package:
S307.217TAu (478 kt) or 300 Kgs. Conventional

Reconnaissance Package:
300 Kgs sensors, cameras & equipment

Launch Weight:
4,430 Kgs (9,766.5 Lbs)

Powerplant:
2x Solid-Fuel Boosters, 455 kN total for 5 Seconds, & 1x 17 kN Ramjet Sustainer

Performance:

Rated Performance:
6,180 Km (3,840 miles) in 1 Hour, 16 Minutes @ 4,840 Km/H (Mach 3.92)

Service Ceiling & Climb Rate:
30,750 meters (100,886') in *REDACTED* @ *REDACTED*

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact AESA

APAx4.1500F "Altair"
Classification:
Synthetic Aperture Imaging Radar, 4-Beam Processing, 110° FFOV

Operation Mode:
X-Band AESA, 1,500W ERP, 45 Hz Update Speed

Design Spec:
400 Km Detection Range, 600 Simultaneous Tracks

Notes:
ECM Resistant, All-Weather Air & Surface Surveillance

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Description:

The "Meduza" drone is the result of a multinational requirement for a very high-altitude observation drone capable of sustained flight over a 6,000 kilometer distance at Mach 3. The Meduza drone is referred to as VBSR-DV308 in Aldarminian nomenclature. Extended flight times at very high speed and moderate altitudes requires active cooling which in turns requires high electrical power; like a large frame missile, the HASR generates its own electrical power by harnessing waste heat from the rocket-augmented scramjet engine to power the drone's avionics, reconnaissance equipment and electrothermal cooling plates which are installed in the aircraft's Carbon Fiber-Reinforced Polymer skin. The Meduza drone is built on a titanium honeycomb frame, layered with CFRP to produce extremely strong, lightweight and high temperature resistant parts. The Meduza drone is launched by electromagnetic Linear Induction Motor, which accelerates the drone along a Mag-Lev track to the SCRAMJET's optimum ignition velocity at a supersonic 1,300 Km/H. The very long LIM length required precludes launching from naval ships, but the drone can be launched from a suborbital platform and allowed to freefall to its ignition velocity. Because of its small size, high altitude and very high speed, the Meduza drone is extremely difficult to intercept with all but the most powerful high-speed missiles. It is intended to test highly defended airspace and observe how a hostile force reacts to enemy overflight without risking the lives of any crewmembers. The Meduza drones are in serial production for foreign contracts primarily, but a few are in use with the Marquesan Armed Forces. HAS.R48 carries a highly advanced 1,500 watt "Altair" X-band radar, one of the most powerful such radars ever fitted to a drone aircraft. The power of the radar affords tremendous versatility; it scans three bands simultaneously along the X band on pseudorandom frequencies, shifting at the radar's update rate of 30 Hz; this makes the probability of intercept or successful jamming extremely low, while the HAS.R48 can maintain as many as 600 simultaneous high speed air tracks, or produce intensely clear, wide-area SAR images of the ground. In addition, a sophisticated electro-optical observation blister on the bottom of the Meduza drone's nose permits downward-looking and forward observation with a day/night, all-weather thermal camera, which colocates a dual-band M/WIR sensor with a 10 megapixel visible light camera behind a 40x telephoto power zoom lens. Even at very high altitudes, the boosted thermal camera automatically corrects for atmospheric obscurants and changing light levels to provide crystal-clear images at ultra high defintion resolutions.

Flyaway Cost Per Unit:(Place orders Here.)
125,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 8:13 am, edited 13 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
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Civil Rights Lovefest

LOA.R70R2 "Archon"

Postby Marquesan » Wed Dec 09, 2020 9:34 am


Image

Nomenclature: LOA.R70R2 "Archon"
Classification:
Low Observable Aggressor Drone

Nation of Origin:
The Marquesan Union, Esvanovia

Date Proposed:
June 6th, 1987

First Flight:
January 1st, 2006

Program Cost:
5,000,000,000 NSD

Number Built:
500

Specifications:

Overall Length:
13.85 meters (45'5")

Tail Height:
2.15 meters (7')

Wings-Folded Height:
3.82 meters (12'6")

Folded Wingspan:
10.60 meters (34'9")

Spread Wingspan:
22.80 meters (74'10")

Wing Area:
55.60 m2 (598.47 ft2)

Wing Loading:
126.97 Kg/m2 (26 Lbs/ft2)

Empty Weight:
2,690 Kgs (5,930.44 Lbs)

Internal Fuel:
3,546.4 liters - 2,890 Kgs (6,371.36 Lbs)

Gross Weight:
5,580 Kgs (12,301.79 Lbs)

Payload Capacity:
1,480 Kgs (3,262.84 Lbs)

Launch Weight:
7,060 Kgs (15,564.64 Lbs)

Powerplant:
2x MTE47.94 Compact Mid-Bypass Turbofans

Rated Thrust:
32.3 kN @ Military Power

Thrust-to-Weight Ratio:
0.93:1 @ MTOW (kgf/kg)

Fuel Burn:
0.13 Kg/Sec @ Cruise, 0.55 Kg/Sec @ Maximum

Performance:

Cruising Performance:
3,700 Km (2,299 miles) in 5 Hours, 45 Minutes @ 645 Km/H (400.78 MPH)

Maximum Performance:
1,430 Km (888.56 miles) in 1 Hour, 27 Minutes @ 980 Km/H (608.94 MPH)

Service Ceiling & Climb Rate:
16,200 meters (53,149') in *REDACTED* @ *REDACTED*

Armaments:

Hardpoints:
4x Internal, 4x External @ 185 Kgs each for missiles & bombs

Systems:

Command & Control:
Testudo Mk. IV Combat Management System

Satellite-Independent Communications:(LOS/NLOS Frequency-Adaptive, 30Hz-30GHz, Encrypted)
1x 10kW PSiAN (SANMEN Communications Suite)

Electronic Warfare Suite:(+/- 40 dB Gain, Frequency-Learning)
2x AES.40 Broadband Adaptive Jamming Suite

Thermal Signature Management:
Thermoelectric Skin Cooling (Adaptive Camouflage)

"Kanaloa" TIMU
Components:
Ring-Laser Gyroscope, Master Clock, Accelerometers/Magnetometers

Operation:
6-Axis Real-Time Measurement of Altitude/Distance/Heading/Movement

Design Spec:
EMP-Hardened, Low Power Consumption, Compact AESA

APAx.10F "Deneb"
Classification:
Synthetic Aperture Imaging Radar

Operation Mode:
X-Band, 10W ERP, 20 Hz Update Speed

Design Spec:
10,000 Meters Imaging Range, 0.5 Meter Resolution @ 10 Km Altitude

Notes:
Ultralight Fire Control Radar, 55° Fixed Field of View

AMPI.aLR "Aquila"
Airborne Stare & Scan Targeting System (EOTS)

Dual-Band M/LWIR Focal Plane Array Sensor, 10 Megapixel, 60° Field-of-View, Upper Cockpit Mounted

Low Light Level Daylight Camera, 10 Megapixel, 75° Field-of-View

1-40x Power-Telephoto Zoom Lens, Electrothermally Cooled Rotating Ball, 45°/Sec Traverse

InGaAs System-on-Chip Targeting Computer, Designation Range: 12m - 60,000m

+ 3D Laser Scanner: 1550nm/658nm Dual Axis Compensation, 10km Max Range

+ Eyesafe Laser Rangefinder: 1570nm 30hz, 10ns Pulse Duration

+ Eyesafe Laser Designator: 1064nm 8-20hz

+ Laser Spot Detector, 190° Wide Angle, Passive Multiple-Target, 0.5 μm - 1.65 μm

Description:

The "Kharon" Pathfinder drone is a compact, supersonic observation drone intended to be flown into extremely hostile areas before an attack to mark the locations of threats and targets. While unarmed, the extremely stealthy drone carries the APAx.10F "Deneb" fixed-mounted AESA radar in its nose. The Deneb radar benefits from the latest advances in solid-state power systems and EMP-hardened scalar supercomputing; it is one of the physically smallest radars in its class produces stunningly clear SAR images of ground targets at 20 Hz. A rotating Aquila Optronics Pod is mounted in the lower nose of the PFC.R49, which colocates a dual-band M/WIR sensor with a 10 megapixel visible light camera, aligned together on a 40x telephoto power zoom lens. These sensors work together to automatically correct for all light conditions and atmospheric obscurants such as dust, fog, rain or oil smoke. The all-weather, day/night optronics system and X-band radar together produce extremely clear, fused broadband images of targets on the ground and provides extremely reliable identification of ground targets while having an extremely low probability of detection or jamming. Kharon drones have a full suite of battlefield lasers and laser receivers which allow the drone to mark targets for laser-guided munitions, designed to interface with the Varuna rocket in specific to destroy disguised targets on the ground, even in the presence of thermal camouflage. Inertial guidance is provided by the "Kanaloa" Timing & Inertial Measurement unit, a GPS-independent guidance system which delivers the drone from waypoint to waypoint without requiring a satellite uplink with pinpoint accuracy. The drone's onboard System-On-Chip "SparkRED" computer places 64 cores and two terabytes of onboard memory on a single chip housed in the TIMU. The high autonomy permitted by the system allows the pathfinder drone to continue its mission even in fully communications-denied environments, relaying information back once out of jamming range. The PFC.R49 drone is built on a titanium honeycomb frame, built up with layers of Carbon Fiber Reinforced-Polymer; this construction method permits an extremely stealthy shape with a very low parts count and precise, blended lines contributing to low observability. The small, mid-bypass turbofan engine developed from business jet turbines has a dorsal intake with a serpentine duct that obscures the bypass fan from radar. The engine's high pressure design blends jet exhaust with the ambient air in a trough behind the jet nozzle lined with heat-absorbent tiles, dramatically decreasing the drone's thermal signature to seekers below the drone. Kharon class drones can fly in terrain-following profiles or can follow high altitude waypoints or any combination dependent on the mission profile. The class is rated with a 2,000+ kilometer combat radius and is capable of supercruising just above the speed of sound in high altitude flight near its service ceiling. As a pathfinder drone, it is capable of marking hundreds of targets during its flight time and relaying that information back to the launching platform. In a loitering flight plan, the PFC.R49 drone uses its three 1,550nm battlefield lasers to mark targets for incoming munitions such as rocket artillery or subsonic cruise missiles, dramatically improving the accuracy of those weapons when a Kharon drone is loitering in the area. The drones are launched from an electromagnetic catapult with a 10 meter Linear Induction Motor. These catapults, much smaller than those on larger Fleet Aircraft Carriers are mounted to "Galeru" GMC.176 class Guided Missile Cruisers in pairs to allow for simultaneous launch; the drones land on shortened runways with arrestor cables on either side of the vessel's Hot Canister Launch cells.

Flyaway Cost Per Unit:(Place orders Here.)
35,000,000 NSD.

Reference Material:
Last edited by Marquesan on Mon Nov 13, 2023 8:29 am, edited 9 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
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Marquesan
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HST.267 "Danava"

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Last edited by Marquesan on Sun Mar 17, 2024 4:20 am, edited 27 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
18 years of stories deleted
Kraven Prevails!

User avatar
Marquesan
Minister
 
Posts: 2247
Founded: Oct 21, 2010
Civil Rights Lovefest

SET.72 "Nosferatu"

Postby Marquesan » Sun Dec 11, 2022 7:23 am

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Last edited by Marquesan on Sun Mar 17, 2024 4:19 am, edited 17 times in total.
"Just so Summanus, wrapped in a smoking whirlwind of blue flame, falls upon people and cities." - John Milton, In Quintum Novembris

@Marquesan I hereby proclaim you as the Gothic Mad Scientist, who actually isn't mad but a brilliant genius which every nations military goes to consult when they quietly tell their leaders, "We'll consult our experts" and when asked who they always say "private sources"
@Marquesan I will say man you're the only person on NS I've ever mistaken for a genuine Weapons designer.
Friend of Kraven, 2005-2023
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