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Shuttle NAR A-2
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Gross Mass: 395,011 kg (870,850 lb). Empty Mass: 121,542 kg (267,954 lb). Thrust (vac): 5,256.893 kN (1,181,797 lbf). Isp: 459 sec. Burn time: 231 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 6.71 m (22.01 ft). Span: 44.51 m (146.03 ft). Length: 61.59 m (202.06 ft). Country: USA. No Engines: 2. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Faget Straight Wing Configuration - Cross Range 2,000 km
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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