F-9 Ashavan II
From MicrasWiki
| Diagram of an early production variant F-9 Ashavan II circa 1676 AN | |
| Type | Air Superiority Fighter |
|---|---|
| Place of origin |
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| Introduced | 1676 AN |
| Designed | 1675 AN |
| Manufacturer | Mistra Aerospace |
| 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) |
| Combat range | 800 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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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.
Operators
ESB Operational Conversion Squadron 8
Raspur Pact
Imperial Constancian Armed Forces 64
Drak-Modani Defense Force 54
Union Defence Force 930
Florian Air Force 175
Grand Army of Ransenar 320
Sanaman Air Force 380
Sanaman Navy (F-9N) 84
Imperial Forces 40
Black Legions 1,456
Self-Defence Forces (Elwynn & Amokolia) 501
Former operators
Sovereign Defence Force – 75 airframes transferred to the Black Legions upon disestablishment
Versions
F-9N Ashavan II
A VTOL version of the F-9 Ashavan II originating in Sanama for use on aircraft carriers and amphibious transport docks as well as the Logistic Support Vessel.