Aerojet General X-8
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The Aerojet General X-8 was an unguided, spin-stabilized sounding rocket designed to launch a 150 pound (68 kg) payload to 200,000 feet (61 km). The X-8 was later spun-off into the prolific Aerobee rocket.
At launch, an 18,000 pound force (80 kN) thrust Aerojet solid rocket booster fired for 2.5 seconds. After booster jettison, a 2,600 pound force (12 kN) thrust RTV-N10 liquid fuel rocket burned for up to 40 seconds (depending on desired apogee). The spent rocket then fell back in a ballistic arch, the payload returning to Earth via parachute. The baseline X-8 measured 20.2 feet (6.2 m) in length and measured 5.25 feet (1.6 m) across the fins. In testing, a maximum altitude of 138 miles (222 km) and a speed of Mach six were achieved.
X-1 · X-2 · X-3 · X-4 · X-5 · X-6 · X-7 · X-8 · X-9 · X-10 · X-11 · X-12 · X-13 · X-14 · X-15 · X-16 · X-17 · X-18 · X-19 · X-20 · X-21 · X-22 · X-23 · X-24 · X-25 · X-26 · X-27 · X-28 · X-29 · X-30 · X-31 · X-32 · X-33 · X-34 · X-35 · X-36 · X-37 · X-38 · X-39 · X-40 · X-41 · X-42 · X-43 · X-44 · X-45 · X-46 · X-47 · X-48 · X-49 · X-50 · X-51 · X-53
See also List of experimental aircraft