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Javelin F-21 Heavenscream

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Javelin F-21 Heavenscream
File:F-21-Heavenscream.png
Javelin F-21 Heavenscream
Type STOVL Strike Fighter
Place of origin Nouvelle Alexandrie Nouvelle Alexandrie
Designed
Manufacturer Javelin Industries
Crew 1
Length 15.6 m
Wingspan 10.7 m
Height 3.6 m
Wing area 42.7 m2
Empty weight 14,700 kg
Loaded weight 22,000 kg
Fuel weight 6,100 kg
Max takeoff weight 27,200 kg
Powerplant 1x variable cycle turbofan, 205 kN
Powerplant 1x lift turbofan, 71 kN
Maximum speed Mach 1.8
Combat radius 1,100 km
Ferry range 2,220 km
15,000 m
Rate of climb 250 m/s
Wing loading 515 kg/m2
Thrust/weight 0.95 (loaded weight with 100% fuel)
Maximum G-loading +7.0/-3.0 g
Armament

Air-to-Air Loadout:

Air-to-Ground Loadout:

Hardpoints:

  • 6x underwing pylons, 6800 kg total
Avionics
  • X band AESA Radar
  • Electro-Optical Sensor System
  • Multispectral Distributed Aperture System
  • Multi-Purpose Passive Receiver System
  • Fiber-Optic Towed Decoy Countermeasure System
  • CNI System

The Javelin F-21 Heavenscream fulfils the requirement for a "short take-off vertical landing" (STOVL) fighter capable of operating from the Behaurnais-class amphibious assault ship, or the Rhodondra-class amphibious assault ships that presently comprise the majority of "flat-top" aviation carrying vessels in the navies of the Raspur Pact.

Development & production timeline

  • 20.I.1700 AN: qty x4 F-21 Heavenscream ordered for evaluation by the Federal Air Force in a contract valued at xxxx écu. Prototypes to be delivered by no later than 1706 AN.