This page no longer updated from 31 October 2001. Latest version can be found at Shuttle NAR A-2

Gross Mass: 395,011 kg. Empty Mass: 121,542 kg. Thrust (vac): 536,054 kgf. Isp: 459 sec. Burn time: 231 sec. Propellants: Lox/LH2 Isp(sl): 359 sec. Diameter: 6.7 m. Span: 44.5 m. Length: 61.6 m. Country: USA. No Engines: 2. SSME Study Status: Study. Comments: Faget Straight Wing Configuration - Cross Range 2,000 km.
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Last update 12 March 2001.
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© Mark Wade, 2001 .