This page no longer updated from 31 October 2001.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

Gross Mass: 1,995,800 kg. Empty Mass: 199,600 kg. Thrust (vac): 2,911,600 kgf. Isp: 267 sec. Burn time: 162 sec. Propellants: N2O4/UDMH Isp(sl): 245 sec. Diameter: 6.6 m. Span: 9.3 m. Length: 57.2 m. Country: USA. No Engines: 1. PF N204/UDMH-2912k Status: Study 1967. Comments: 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/UDMH Propellant engine, HY-140 Hull.
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Last update 12 March 2001.
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© Mark Wade, 2001 .