This page no longer updated from 31 October 2001.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

Manufacturer Name: AJ-260X. Designer: Aerojet. Used on stages: 260 inch solid FL, MLLV-0, Saturn LCB-SR. Used on launch vehicles: MLLV, Saturn INT-05A, Saturn LCB-SR, Saturn V-D, Saturn V/4-260. Gross Mass: 1,648,355 kg. Empty Mass: 156,126 kg. Propellants: Solid Thrust(vac): 3,608,918 kgf. Thrust(vac): 35,390.70 kN. Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 114 sec. Diameter: 6.6 m. Length: 30.5 m. Chambers: 1. Country: USA. Status: Developed to 1966. Comments: Proposed for use in various Saturn and Nova configurations. Full length version of 260 inch motor tested in 1960's.
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Last update 12 March 2001.
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© Mark Wade, 2001 .