This page no longer updated from 31 October 2001. Latest version can be found at Shuttle DC-3-2

Gross Mass: 199,238 kg. Empty Mass: 54,422 kg. Thrust (vac): 300,000 kgf. Isp: 459 sec. Burn time: 218 sec. Propellants: Lox/LH2 Isp(sl): 359 sec. Diameter: 4.5 m. Span: 27.7 m. Length: 37.4 m. Country: USA. No Engines: 1. SSME Study Status: Study. Comments: Faget Configuration - Cross Range 323 km.
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Last update 12 March 2001.
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© Mark Wade, 2001 .