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Shuttle NAR A-1
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Gross Mass: 1,641,723 kg (3,619,379 lb). Empty Mass: 273,469 kg (602,895 lb). Thrust (vac): 28,130.189 kN (6,323,918 lbf). Isp: 442 sec. Burn time: 208 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 9.88 m (32.41 ft). Span: 74.39 m (244.06 ft). Length: 85.37 m (280.08 ft). Country: USA. No Engines: 11. 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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