This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-IC-4(S)B

Gross Mass: 2,875,500 kg. Empty Mass: 154,000 kg. Thrust (vac): 3,948,100 kgf. Isp: 304 sec. Burn time: 206 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 50.6 m. Country: USA. No Engines: 5. F-1 Status: Study Boeing 1967. Comments: S-IC with 336 inch stretch, 6,000,0000 lbs propellant, structural strength increased from 56% to 65% depending on station, resulting in 13.9% increase in empty weight.
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Last update 12 March 2001.
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© Mark Wade, 2001 .