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Spacemaster-1
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Gross Mass: 1,224,490 kg (2,699,530 lb). Empty Mass: 203,342 kg (448,292 lb). Thrust (vac): 28,082.538 kN (6,313,206 lbf). Isp: 442 sec. Burn time: 155 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 8.00 m (26.20 ft). Span: 45.12 m (148.03 ft). Length: 57.93 m (190.05 ft). Country: USA. No Engines: 14. Engine: SSME Study. Status: Study 1967. First Flight: 1978. Unique Catamaran configuration.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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