Saturn LCB-Storable-250 stage (original) (raw)

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Saturn LCB-Storable-250 stage

Part of Saturn LRB stage series

N2O4/UDMH propellant rocket stage. 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, Ni-250 Hull.

AKA: Saturn LCB-Storable-250. Status: Study 1967. Thrust: 21,232.30 kN (4,773,211 lbf). Gross mass: 1,451,500 kg (3,200,000 lb). Unfuelled mass: 108,900 kg (240,000 lb). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 163 s. Height: 40.70 m (133.50 ft). Diameter: 6.61 m (21.68 ft). Span: 9.26 m (30.38 ft).

Country: USA. Engines: PF N204/UDMH-2165k. Launch Vehicles: Saturn LCB-Storable-250. Propellants: N2O4/UDMH.

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