This page no longer updated from 31 October 2001.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

Manufacturer Name: AJ10-118D. Designer: Aerojet. Used on stages: Delta D. Used on launch vehicles: Delta B, Delta C, Delta D. Propellants: Nitric acid/UDMH Thrust(vac): 3,436 kgf. Thrust(vac): 33.70 kN. Isp: 278 sec. Isp (sea level): 160 sec. Burn time: 170 sec. Mass Engine: 90 kg. Diameter: 0.8 m. Chambers: 1. Chamber Pressure: 7.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 38.18. Country: USA. Status: Out of Production. First Flight: 1962. Last Flight: 1969. Flown: 27.
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Last update 12 March 2001.
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© Mark Wade, 2001 .