This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Manufacturer Name: AJ10-118F. Designer: Aerojet. Used on stages: Delta F. Used on launch vehicles: Delta 100, Delta 1914, N-2. Propellants: Nitric acid/UDMH Thrust(vac): 4,218 kgf. Thrust(vac): 41.40 kN. Isp: 306 sec. Burn time: 335 sec. Mass Engine: 95 kg. Diameter: 1.4 m. Chambers: 1. Chamber Pressure: 9.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 44.40. Country: USA. Status: Out of Production. First Flight: 1972. Last Flight: 1987. Flown: 20.
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Last update 12 March 2001.
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© Mark Wade, 2001 .