Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Sud-Ouest SO 9000 (Trident I) Military Research / Interceptor Aircraft.
2 x Turbomeca "Marbore II" turbojet engines at wingtips developing 882lb thrust each with fuselage-mounted 1 x SEPR 481 rocket motor developing 9,920lb of thrust.
Propulsion
1,059 mph
1,705 kph | 921 kts
Max Speed
32,808 ft
10,000 m | 6 miles
Service Ceiling
5,700 ft/min
1,737 m/min
Rate-of-Climb