This page no longer updated from 31 October 2001. Latest version can be found at Saturn S-II-C3

Gross Mass: 204,044 kg. Empty Mass: 24,938 kg. Thrust (vac): 362,745 kgf. Isp: 420 sec. Burn time: 200 sec. Propellants: Lox/LH2 Isp(sl): 300 sec. Diameter: 8.3 m. Span: 8.3 m. Length: 21.3 m. Country: USA. No Engines: 4. J-2 Status: Study 1960.
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Last update 12 March 2001.
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© Mark Wade, 2001 .