This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 1,542,200 kg.
Empty Mass: 154,200 kg. Thrust (vac): 2,300,800 kgf. Isp: 280 sec. Burn time: 166 sec. Propellants: N2O4/Alumizine Isp(sl): 260 sec. Diameter: 6.6 m. Span: 9.3 m. Length: 36.3 m. Country: USA. No Engines: 1. PF N204/Alumizine-2300k 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/Alumizine Propellant engine, HY-140 Hull.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .