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Saturn II C-5A
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Gross Mass: 384,057 kg (846,700 lb). Empty Mass: 31,740 kg (69,970 lb). Thrust (vac): 4,446.648 kN (999,646 lbf). Isp: 420 sec. Burn time: 320 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). Length: 21.39 m (70.17 ft). Country: USA. No Engines: 5. Engine: J-2. Status: Study 1961. Used as: Saturn C-5A-2; Saturn C-4B-2; Saturn C-3B-2. Final common second stage design for Saturn C-3, C-4 and C-5 (November 1961). Developed into Saturn V second stage.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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