This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 561,100 kg.
Empty Mass: 57,600 kg. Thrust (vac): 1,136,300 kgf. Isp: 263 sec. Burn time: 114 sec. Propellants: Solid Isp(sl): 238 sec. Diameter: 6.6 m. Span: 6.6 m. Length: 21.7 m. Country: USA. No Engines: 1. AJ-260X 1/3 Status: Development 1968. Comments: 260 inch solid booster - full length.
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Last update 12 March 2001.
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© Mark Wade, 2001 .