This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 952,500 kg.
Empty Mass: 68,000 kg. Thrust (vac): 1,583,900 kgf. Isp: 304 sec. Burn time: 167 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 6.6 m. Span: 10.6 m. Length: 36.4 m. Country: USA. No Engines: 2. F-1 Status: Hardware. Comments: Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb pyld to LEO): S-IC Technology Liquid Booster: 260 inch liquid booster with 2 x F-1 engines, recoverable/reusable.
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Last update 12 March 2001.
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© Mark Wade, 2001 .