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Mini-shuttle
Part of Shuttle
American manned rocketplane. Study 1972. In August 1972 it was proposed to test a subscale version of the shuttle to test the aerodynamics. The 13,750 kg vehicle would be 11 m long and have a wingspan of 7 m.
Status: Study 1972. Gross mass: 13,750 kg (30,310 lb). Height: 11.00 m (36.00 ft). Span: 7.00 m (22.90 ft).
Air dropped from an NB-52 carrier aircraft, it would use the XLR-99 engine developed for the X-15 to boost it to over Mach 5.
It would be equipped with off-the-shelf on-board systems, but use the thermal protection materials planned for the shuttle. Proponents said they could accomplish the program for $19.7 million, but opponents said it would cost over $150 million. It was never authorized, and it was only on the first orbital flight that the shuttle aerodynamics were proven at supersonic speeds.
Family:
Rocketplane,
Suborbital,
US Rocketplanes.
Country:
USA.
Engines:
XLR99.
Propellants:
Lox/Ammonia.
Agency:
North American.
Bibliography:
44.
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