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Saturn LCB-Lox/RP-1
Part of Saturn I
American orbital launch vehicle. Boeing Low-Cost Saturn Derivative Study, 1967 (trade study of 260 inch first stages for S-IVB, all delivering 86,000 lb payload to LEO): Low Cost Booster, Single Pressure-fed LOx/RFP-1 engine.

Status: Study 1967. Payload: 39,000 kg (85,000 lb). Thrust: 18,682.10 kN (4,199,903 lbf). Gross mass: 1,526,400 kg (3,365,100 lb). Height: 80.00 m (262.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

LEO Payload: 39,000 kg (85,000 lb) to a 185 km orbit at 28.00 degrees.

Stage Data - Saturn LCB-Lox/RP-1



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: PF RP-1. Stages: Saturn IVB (S-IB), Saturn LCB-Lox/RP-1 stage.

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