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Shuttle MDC-A-1
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Gross Mass: 1,242,630 kg (2,739,530 lb). Empty Mass: 220,254 kg (485,576 lb). Thrust (vac): 18,956.000 kN (4,261,478 lbf). Isp: 442 sec. Burn time: 230 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 8.00 m (26.20 ft). Span: 46.04 m (151.04 ft). Length: 59.45 m (195.04 ft). Country: USA. No Engines: 10. Engine: SSME Study. Status: Study 1969. Cost $ : 30.000 million. First Flight: 1978. Delta winged configuration.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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