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Shuttle R134C-2
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Gross Mass: 424,449 kg (935,749 lb). Empty Mass: 138,910 kg (306,240 lb). Thrust (vac): 4,804.130 kN (1,080,011 lbf). Isp: 459 sec. Burn time: 264 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 4.57 m (14.99 ft). Span: 37.80 m (124.00 ft). Length: 64.02 m (210.03 ft). Country: USA. No Engines: 2. 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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