This page no longer updated from 31 October 2001. Latest version can be found at Saturn S-IC-8

Gross Mass: 3,627,500 kg. Empty Mass: 181,400 kg. Thrust (vac): 6,314,600 kgf. Isp: 304 sec. Burn time: 157 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 12.2 m. Span: 22.9 m. Length: 48.8 m. Country: USA. No Engines: 8. F-1 Status: Study 1960.
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Last update 12 March 2001.
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© Mark Wade, 2001 .