F-9 Ashavan II
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Diagram of the F-8M variant circa 1672 AN | |
Type | Air Superiority Fighter |
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Place of origin | Talenore / Raspur Pact |
Introduced | 1676 AN |
Designed | 1675 AN |
Manufacturer | Mistra Aerospace (Allied Production Matrix) |
Length | 14.5 m |
Wingspan | 8.9 m |
Empty weight | 8,160 kg |
Loaded weight | 16,800 kg |
Powerplant | 1 × Mistra RM7 afterburning turbofan engine |
Maximum speed | 2,214 km/h (Mach 2.08) |
Sortie range | 640 km |
Ferry range | 2,560 km |
Service ceiling | 13,716 m |
Rate of climb | 318 m/s |
Armaments |
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Defensive measures |
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Avionics |
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