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Saturn IC C-3B
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Gross Mass: 1,160,787 kg (2,559,097 lb). Empty Mass: 72,549 kg (159,943 lb). Thrust (vac): 22,954.798 kN (5,160,444 lbf). Isp: 304 sec. Burn time: 140 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). Length: 34.41 m (112.89 ft). Country: USA. No Engines: 5. Engine: F-1. Status: Study 1961. Used as: Saturn C-3B-1. Final first stage design of Saturn C-3 (November 1961).
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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