This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .