F-9 Ashavan II: Difference between revisions
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The '''{{PAGENAME}}''' is an air superiority fighter developed from the [[FA-9 Banshee]], retaining the basic airframe and turbofan engine of the originating platform whilst undergoing extensive internal modification to establish backwards compatibility with the avionics and weaponry of the [[Raspur Pact]] - the new aircraft's primary intended export customer and licencee. | |||
[[Category:Weaponry]][[Category:Raspur Pact]] | [[Category:Weaponry]][[Category:Raspur Pact]] | ||
Revision as of 08:38, 17 August 2019
 Diagram of the F-8M variant circa 1672 AN | |
| Type | Air Superiority Fighter |
|---|---|
| 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 |
|
The F-9 Ashavan II is an air superiority fighter developed from the FA-9 Banshee, retaining the basic airframe and turbofan engine of the originating platform whilst undergoing extensive internal modification to establish backwards compatibility with the avionics and weaponry of the Raspur Pact - the new aircraft's primary intended export customer and licencee.
