This page no longer updated from 31 October 2001. Latest version can be found at AJ-260X 1/3

Manufacturer Name: AJ-260X 1/3. Designer: Aerojet. Used on stages: Saturn 3S-2. Propellants: Solid Thrust(vac): 1,136,300 kgf. Thrust(vac): 11,143.00 kN. Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 114 sec. Chambers: 1. Country: USA. Status: Design concept 1960's.
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Last update 12 March 2001.
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© Mark Wade, 2001 .