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Gross Mass: 952,500 kg (2,099,900 lb). Empty Mass: 68,000 kg (149,000 lb). Thrust (vac): 15,532.700 kN (3,491,890 lbf). Isp: 304 sec. Burn time: 167 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 6.61 m (21.68 ft). Span: 10.58 m (34.71 ft). Length: 36.36 m (119.29 ft). Country: USA. No Engines: 2. Engine: F-1. Status: Study 1967. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb pyld to LEO): S-IC Technology Liquid Booster: 260 inch liquid booster with 2 x F-1 engines, recoverable/reusable
Used on Launch Vehicles:
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