This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-IC-1A

Gross Mass: 2,694,700 kg. Empty Mass: 160,600 kg. Thrust (vac): 4,735,900 kgf. Isp: 304 sec. Burn time: 160 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 48.2 m. Country: USA. No Engines: 6. F-1 Status: Study 1966. Comments: Basic Saturn IC stretched 240 inches with 6 F-1 engines.
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Last update 12 March 2001.
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© Mark Wade, 2001 .