This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 1,648,355 kg.
Empty Mass: 156,126 kg. Thrust (vac): 3,608,918 kgf. Isp: 263 sec. Burn time: 114 sec. Propellants: Solid Isp(sl): 238 sec. Diameter: 6.6 m. Span: 6.6 m. Length: 30.5 m. Country: USA. No Engines: 1. AJ-260X Status: Devel. Comments: 260 inch solid booster - full length. These would have been the flight configuration motors, replacing the Saturn V first stage or being used as booster motors in various Uprated Saturn and Nova configurations.
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Last update 12 March 2001.
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© Mark Wade, 2001 .