F-17 Axarana
From MicrasWiki
| Diagram of an early production variant F-9 Ashavan II circa 1676 AN | |
| Type | Sixth generation air superiority fighter |
|---|---|
| Place of origin |
|
| Introduced | 1697 AN |
| Designed | 1688–1697 AN |
| Manufacturer | Brightworks Mistra and various others |
| Length | 16 m |
| Wingspan | 11.5 m |
| Empty weight | 13,500 kg |
| Loaded weight | 23,000 kg |
| Powerplant | 2 × AIC afterburning turbofan engines with thrust vectoring |
| Maximum speed | Minimum 4,500 km/h |
| Combat range | 1,400 km |
| Ferry range | 3,200 km |
| Service ceiling | 18,000 m |
| Rate of climb | 400 m/s |
| Armaments |
|
| Avionics | Classified |
| Electronics | Classified |
| Other | Drone swarm capability |
The F-17 Axarana is a sixth generation fighter jointly developed by Brightworks Mistra, Neridia Defense Industries, Simines, Gaelen Technologies Corporation, Eclipse, Dingo Enterprises, ESB, Farrar International and Javelin Industries for the Raspur Pact. Development began in 1688 and the aircraft made its first operational flight in 1697. Deployment is expected from 1698 and onwards.