Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dassault Mirage IIING Supersonic Single-Seat Fighter Prototype.
1 x SNECMA Atar 9K-50 afterburning turbojet engine developing 15,873lb of thrust.
Propulsion
1,320 mph
2,125 kph | 1,147 kts
Max Speed
57,005 ft
17,375 m | 11 miles
Service Ceiling
8,635 ft/min
2,632 m/min
Rate-of-Climb