F-9 Ashavan II
From MicrasWiki
Jump to navigationJump to search
Diagram of an early production variant F-9 Ashavan II circa 1676 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 |
|
Defensive measures |
|
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.
Operators
- ESB Operational Conversion Squadron 8
- Raspur Pact
- Imperial Constancian Armed Forces 20/64 (on order)
- Drak-Modani Defense Force 54
- Union Defence Force 157/432 (on order)
- Florian Air Force 175
- Grand Army of Ransenar 200/320 (on order)
- Sanaman Air Force 140
- Imperial Forces 40
- Black Legions 239/1,456 (on order)
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.