This page no longer updated from 31 October 2001.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

Gross Mass: 874,100 kg. Empty Mass: 18,100 kg. Thrust (vac): 1,579,200 kgf. Isp: 304 sec. Burn time: 162 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 6.6 m. Span: 6.6 m. Length: 47.9 m. Country: USA. No Engines: 2. F-1 Status: Study Boeing 1967. Comments: Liquid rocket booster strap-ons using 2 F-1's.
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Last update 12 March 2001.
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© Mark Wade, 2001 .