F-9 Ashavan II

From MicrasWiki
Revision as of 08:27, 17 August 2019 by Continuator (talk | contribs) (Created page with "{{ infobox | bodyclass = toccolours | bodystyle = float:right; margin: 0 0 1em 1em; font-size: 85%; width: 30em;background-color:#C0C0C0;border:1px solid #FFD700; | titl...")
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
Jump to navigationJump to search
F-9 Ashavan II
F-9 Ashavan II.png
Diagram of the F-8M variant circa 1672 AN
Type Air Superiority Fighter
Place of origin Talenore 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
  • ES-13 radar warning receiver
  • ES-14 RF countermeasures
  • ES-24: chaff jamming countermeasure system
Avionics
  • ES-27 "Froyalan" radar