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Gross Mass: 1,678,300 kg.
Empty Mass: 136,100 kg. Thrust (vac): 2,756,800 kgf. Isp: 263 sec. Burn time: 144 sec. Propellants: Solid Isp(sl): 238 sec. Diameter: 6.6 m. Span: 9.3 m. Length: 38.1 m. Country: USA. No Engines: 1. AJ-260X 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, Solid Propellant.
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Last update 12 March 2001.
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© Mark Wade, 2001 .