This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Manufacturer Name: AJ10-104. Designer: Aerojet. Used on stages: Able-Star, Delta 104. Used on launch vehicles: Delta, Thor Able-Star. Propellants: Nitric acid/UDMH Thrust(vac): 3,579 kgf. Thrust(vac): 35.10 kN. Isp: 278 sec. Burn time: 296 sec. Mass Engine: 90 kg. Diameter: 1.4 m. Chambers: 1. Chamber Pressure: 7.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 39.77. Country: USA. Status: Out of Production. First Flight: 1960. Last Flight: 1965. Flown: 32.
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 .