Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the SNCASE S.E.212 (Durandal) Prototype Fighter-Interceptor Aircraft.
1 x SNECMA Atar 101F afterburning turbojet engine developing 9,700 lb of thrust with 1 x SEPR 75 rocket engine devliering and additional 1,653 lb of thrust.
Propulsion
1,035 mph
1,665 kph | 899 kts
Max Speed
39,000 ft/min
11,887 m/min
Rate-of-Climb