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Saturn IVB-A
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Gross Mass: 118,800 kg (261,900 lb). Empty Mass: 12,900 kg (28,400 lb). Thrust (vac): 956.100 kN (214,940 lbf). Isp: 421 sec. Burn time: 450 sec. Propellants: Lox/LH2. Isp(sl): 200 sec. Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft). Length: 17.80 m (58.30 ft). Country: USA. No Engines: 1. Engine: J-2. Status: Study 1965. Douglas Studies, 1965: S-IVB with 215k lbf J-1 (actual final model had 230k J-1)
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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