Javelin F-19 Greystrike: Difference between revisions
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* Communications, Navigation and Identification System | * Communications, Navigation and Identification System | ||
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==Development & production timeline== | |||
*35.XV.{{AN|1699}}: qty x2 F-19 Greystrike ordered for evaluation. Prototypes to be delivered by no later than {{AN|1705}}. | |||
[[Category:Aircraft]] | [[Category:Aircraft]] |
Revision as of 19:51, 31 August 2021
Javelin F-19 Greystrike | |
Type | Air Superiority Fighter |
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Place of origin | Nouvelle Alexandrie |
Designed | |
Manufacturer | Javelin Industries |
Crew | 1 |
Length | 21.0 m |
Wingspan | 15.0 m |
Height | 3.8 m |
Wing area | 95 m2 |
Empty weight | 16,800 kg |
Loaded weight | 29,100 kg |
Fuel weight | 10,800 kg |
Max takeoff weight | 38,700 kg |
Powerplant | 2x adaptive cycle afterburning turbofans, 205 kN each |
Maximum speed |
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Combat radius |
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Ferry range | 5,600 km |
Service ceiling | 22,700 m |
Rate of climb | 470 m/s |
Wing loading | 285 kg/m2 |
Thrust/weight | 1.44 |
Maximum G-loading | +9.5/-3.5 g |
Armament |
Air-to-Air loadout:
Air-to-Ground loadout:
Hardpoints:
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Avionics |
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