(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Dassault S-01 (Prototype) production variant)
1 x SNECMA Atar 9K-50 afterburning turbojet engine developing 15,885lb of thrust.
(2,400 kph | 1,296 kts)
(16,500 m | 10 mi)
(3,350 km | 6,204 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the Dassault S-01 (Prototype) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
2 x 30mm ADEN automatic cannons mounted internally.
Up to 8,818lb of externally-held stores across seven hardpoints to include conventional drop bombs, rocket pods, and jettisonable fuel tanks.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.