This page no longer updated from 31 October 2001.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

Manufacturer Name: AJ-260-1/3. Designer: Aerojet. Used on stages: 260 inch solid TL. Used on launch vehicles: Saturn INT-05B. Propellants: Solid Thrust(vac): 1,030,455 kgf. Thrust(vac): 10,105.00 kN. Isp: 275 sec. Burn time: 130 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 .