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The X-15 had an ejection seat designed to operate at speeds up to Mach 4 (4,500 km/h; 2,800 mph) and/or 120,000 feet (37 km) (23 miles) altitude, although it was never used during the program. [12] In the event of ejection, the seat was designed to deploy fins, which were used until it reached a safer speed/altitude at which to deploy its main ...
Among other things, one of the changes was provisions for a dummy scramjet to test if wind tunnel testing was correct. Unfortunately, on the final flight of the X-15-A2 , the shock waves sent out by the scramjet at Mach 6.7 caused extremely intense heating of over 2,700 °F (1,480 °C). This then drilled into the ventral fin and melted large holes.
Weighing 167 kilograms (368 lb), the 9M330 missile is 3,000 millimetres (9.8 ft) long, carries a 15 kilograms (33 lb) warhead and has a peak speed of around Mach 2.8 (3,430 km/h; 2,130 mph). Using command guidance and radar controlled proximity fuzes , the missiles can maneuver at up to 30 g and engage targets flying at up to Mach 2 (2,500 km/h ...
The suit is a direct descendant of the U.S. Air Force high-altitude pressure suits worn by the two-man crews of the SR-71 Blackbird, pilots of the U-2 and X-15, and Gemini pilot-astronauts, and the Launch Entry Suits (LES) worn by NASA astronauts starting on the STS-26 flight, the first flight after the Challenger disaster.
The Pegasus rocket booster separated from its B-52 carrier at 40,000 feet and its solid rocket took the combination to Mach 10 at 110,000 feet. [9] The X-43A split away at Mach 9.8 and the engine was started at Mach 9.65 for 10–12 seconds with thrust approximately equal to drag, and then glided to the Pacific Ocean after 14 minutes. [9]
F/A-18E/F Super Hornet, EA-18G Growler, F-16, F-15, F-35A/B/C, F-22, P-8A Poseidon, surface ships and submarines (via VLS) The Mako Multi-Mission Hypersonic Missile is a stand-off hypersonic missile developed by Lockheed Martin and CoAspire, specifically designed to fit in the internal weapons bay of the F-35A/C and F-22A .