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Shuttle MDC-A-2
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Gross Mass: 335,601 kg (739,873 lb). Empty Mass: 73,442 kg (161,911 lb). Thrust (vac): 3,070.400 kN (690,253 lbf). Isp: 459 sec. Burn time: 379 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 7.00 m (22.90 ft). Span: 23.08 m (75.72 ft). Length: 32.62 m (107.02 ft). Country: USA. No Engines: 2. Engine: SSME Study. Status: Study 1969. Cost $ : 18.000 million. First Flight: 1978. HL-10 lifting body configuration
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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