Dassault Aviation - France
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Maximum Take-Off Weight
1 x SNECMA (Pratt & Whitney) TF104B turbofan engine developing 19,842lb of thrust; 8 x Rolls Royce RB162 lift engines developing 4,410 lb of thrust each.
(2,520 kph | 1,361 knots)
(17,000 m | 11 miles)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
None. Assumed internal cannons with external provision for air-to-air missiles.