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Saturn LCB-Storable-140 stage
Part of Saturn LRB stage series Family
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, HY-140 Hull.

AKA: Saturn LCB-Storable-140. Status: Study 1967. Thrust: 28,553.00 kN (6,418,969 lbf). Gross mass: 1,995,800 kg (4,399,900 lb). Unfuelled mass: 199,600 kg (440,000 lb). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 162 s. Height: 57.16 m (187.53 ft). Diameter: 6.61 m (21.68 ft). Span: 9.26 m (30.38 ft).



Country: USA. Engines: PF N204/UDMH-2912k. Launch Vehicles: Saturn LCB-Storable-140. Propellants: N2O4/UDMH.

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