Javelin F-21 Heavenscream
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 Javelin F-21 Heavenscream | |
| Type | STOVL Strike Fighter |
|---|---|
| Place of origin |
 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:
|
| Avionics |
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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.
- 1711–1724: 124x delivered into NAX service.
- 1729: 48x ordered by the Imperial Constancian Armed Forces for Fleet Air Arm.
