AJ10-118D Manufacturer Name: AJ10-118D. Designer: Aerojet. Propellants: Nitric acid/UDMH. Thrust(vac): 33.700 kN (7,576 lbf). Isp: 278 sec. Burn time: 170 sec. Mass Engine: 90 kg (198 lb). Diameter: 0.84 m (2.75 ft). Chambers: 1. Chamber Pressure: 7.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 38.18. Country: USA. First Flight: 1962. Last Flight: 1969. Flown: 24. AJ10-118D used on Rocket Stages Used on stage: Delta D. on launch vehicle: Delta B. Used on stage: Delta D. on launch vehicle: Delta C. Used on stage: Delta D. on launch vehicle: Delta D.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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