This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-IC/260

Gross Mass: 2,721,600 kg. Empty Mass: 181,400 kg. Thrust (vac): 3,948,100 kgf. Isp: 304 sec. Burn time: 192 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 42.0 m. Country: USA. No Engines: 5. F-1 Status: Study Boeing 1968. Comments: Standard length S-IC but with feed of propellant from fuel and propellant tanks housed above strap-on solid rocket motors.
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Last update 12 March 2001.
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© Mark Wade, 2001 .