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Shuttle LCR-1
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Gross Mass: 1,512,381 kg (3,334,229 lb). Empty Mass: 286,621 kg (631,891 lb). Thrust (vac): 27,054.517 kN (6,082,097 lbf). Isp: 442 sec. Burn time: 193 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 10.00 m (32.00 ft). Span: 46.04 m (151.04 ft). Length: 75.15 m (246.55 ft). Country: USA. No Engines: 13. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Swept wingd configuration.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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