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Saturn IVB C-3B
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Gross Mass: 52,144 kg (114,957 lb). Empty Mass: 6,801 kg (14,993 lb). Thrust (vac): 889.325 kN (199,928 lbf). Isp: 420 sec. Burn time: 207 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 5.59 m (18.33 ft). Span: 5.59 m (18.33 ft). Length: 15.40 m (50.50 ft). Country: USA. No Engines: 1. Engine: J-2. Status: Study 1961. Used as: Saturn C-3B-3. Final common third stage design for Saturn C-3B (November 1961).
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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