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Saturn LCB-Storable-140
Part of Saturn V
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 N2O4/UDMH Propellant engine, HY-140 Steel Hull.

Status: Study 1967. Payload: 39,000 kg (85,000 lb). Thrust: 26,200.30 kN (5,890,062 lbf). Gross mass: 2,161,400 kg (4,765,000 lb). Height: 90.00 m (295.00 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-Storable-140



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: PF N204/UDMH-2912k. Stages: Saturn IVB (S-IB), Saturn LCB-Storable-140 stage.

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