This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 991,000 kg.
Empty Mass: 89,300 kg. Thrust (vac): 1,571,780 kgf. Isp: 455 sec. Burn time: 900 sec. Propellants: Lox/LH2 Isp(sl): 347 sec. Diameter: 39.0 m. Span: 39.0 m. Length: 39.7 m. Country: USA. No Engines: 7. RS-2200 Status: Design.
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Last update 12 March 2001.
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© Mark Wade, 2001 .