This page no longer updated from 31 October 2001. Latest version can be found at AJ10-118E

Manufacturer Name: AJ10-118E. Designer: Aerojet. Used on stages: Delta E. Used on launch vehicles: Delta E, Delta G, Delta J, Delta L, Delta M, Delta N, N. Propellants: Nitric acid/UDMH Thrust(vac): 3,579 kgf. Thrust(vac): 35.10 kN. Isp: 278 sec. Burn time: 400 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: 1965. Last Flight: 1982. Flown: 57.
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Last update 12 March 2001.
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© Mark Wade, 2001 .