This page no longer updated from 31 October 2001. Latest version can be found at Saturn LCB-Alumizine-140

Family: Saturn I. Country: USA. 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): Low Cost Booster, Single Pressure-fed N2O4/Alumizine Propellant engine, HY-140 Steel Hull.


LEO Payload: 39,000 kg. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 2,136,460 kgf. Total Mass: 1,707,800 kg. Core Diameter: 6.6 m. Total Length: 65.0 m.


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Last update 12 March 2001.
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© Mark Wade, 2001 .