Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dassault S-01 (Prototype) Single-Seat, Single-Engine Strike Fighter Prototype.
1 x SNECMA Atar 9K-50 afterburning turbojet engine developing 15,885lb of thrust.
Propulsion
1,491 mph
2,400 kph | 1,296 kts
Max Speed
54,134 ft
16,500 m | 10 miles
Service Ceiling
2,082 miles
3,350 km | 1,809 nm
Operational Range
16,500 ft/min
5,029 m/min
Rate-of-Climb