This page no longer updated from 31 October 2001. Latest version can be found at Saturn MLV 5-23L-0

Gross Mass: 1,180,000 kg. Empty Mass: 80,000 kg. Thrust (vac): 1,579,000 kgf. Isp: 304 sec. Burn time: 200 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 6.6 m. Span: 6.6 m. Length: 51.0 m. Country: USA. No Engines: 2. F-1 Status: Study 1966. Comments: Liquid strap-on booster studied for improved Saturn V.
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Last update 12 March 2001.
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© Mark Wade, 2001 .