This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Manufacturer Name: AJ10-101. Designer: Aerojet. Used on stages: Able. Used on launch vehicles: Atlas Able, Thor Able. Propellants: Nitric acid/UDMH Thrust(vac): 3,500 kgf. Thrust(vac): 34.30 kN. Isp: 270 sec. Isp (sea level): 240 sec. Burn time: 115 sec. Diameter: 0.8 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1958. Last Flight: 1960. Flown: 20.
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 .