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astronautix.com Saturn IC C-3B


Gross Mass: 1,160,787 kg. Empty Mass: 72,549 kg. Thrust (vac): 2,340,738 kgf. Isp: 304 sec. Burn time: 140 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 34.4 m. Country: USA. No Engines: 5. F-1 Status: Study 1961. Used as: Saturn C-3B-1. Comments: Final first stage design of Saturn C-3 (November 1961).
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Last update 12 March 2001.
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© Mark Wade, 2001 .