AJ-260X 1/3 Manufacturer Name: AJ-260X 1/3. Designer: Aerojet. Propellants: Solid. Thrust(vac): 11,143.000 kN (2,505,046 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 114 sec. Chambers: 1. Country: USA. Status: Design concept 1960's. AJ-260X 1/3 used on Rocket Stages Used on stage: Saturn 3S-2.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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