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Shuttle R134C-1
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Gross Mass: 1,764,039 kg (3,889,040 lb). Empty Mass: 351,538 kg (775,008 lb). Thrust (vac): 28,824.774 kN (6,480,067 lbf). Isp: 442 sec. Burn time: 209 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 10.37 m (34.02 ft). Span: 46.04 m (151.04 ft). Length: 81.40 m (267.00 ft). Country: USA. No Engines: 12. Engine: SSME Study. Status: Study 1970. 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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