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Shuttle LS A-2
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Gross Mass: 406,344 kg (895,835 lb). Empty Mass: 104,891 kg (231,245 lb). Thrust (vac): 6,823.560 kN (1,533,997 lbf). Isp: 459 sec. Burn time: 196 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 8.00 m (26.20 ft). Span: 28.05 m (92.02 ft). Length: 49.70 m (163.00 ft). Country: USA. No Engines: 3. Engine: SSME Study. Status: Study 1969. First Flight: 1978. High-fineness lifting-body configuration. Cross Range 2,419 km
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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