This page no longer updated from 31 October 2001. Latest version can be found at Shuttle NAR A-1

Gross Mass: 1,641,723 kg. Empty Mass: 273,469 kg. Thrust (vac): 2,868,481 kgf. Isp: 442 sec. Burn time: 208 sec. Propellants: Lox/LH2 Isp(sl): 392 sec. Diameter: 9.9 m. Span: 74.4 m. Length: 85.4 m. Country: USA. No Engines: 11. SSME Study Status: Study. Comments: Faget Straight Wing Configuration.
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Last update 12 March 2001.
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© Mark Wade, 2001 .