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Shuttle LCR-2
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Gross Mass: 322,449 kg (710,878 lb). Empty Mass: 120,816 kg (266,353 lb). Thrust (vac): 4,719.636 kN (1,061,016 lbf). Isp: 459 sec. Burn time: 189 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 8.00 m (26.20 ft). Span: 34.70 m (113.80 ft). Length: 45.00 m (147.00 ft). Country: USA. No Engines: 2. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Faget Straight Wing Configuration
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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