This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-IC-23(L)

Gross Mass: 2,694,000 kg. Empty Mass: 169,000 kg. Thrust (vac): 3,946,624 kgf. Isp: 304 sec. Burn time: 192 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 48.1 m. Country: USA. No Engines: 5. F-1 Status: Study NASA 1966. Comments: Basic Saturn IC stretched 240 inches with standard F-1 engines.
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Last update 12 March 2001.
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© Mark Wade, 2001 .