This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 998,000 kg.
Empty Mass: 75,000 kg. Thrust (vac): 1,088,000 kgf. Isp: 428 sec. Burn time: 357 sec. Propellants: Lox/LH2 Diameter: 20.6 m. Span: 20.6 m. Length: 27.1 m. Country: USA. No Engines: 5. J-2 Status: Study General Dynamics 1963. Comments: Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. .
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Last update 12 March 2001.
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© Mark Wade, 2001 .