AJ10-118E Manufacturer Name: AJ10-118E. Designer: Aerojet. Propellants: Nitric acid/UDMH. Thrust(vac): 35.100 kN (7,891 lbf). Isp: 278 sec. Burn time: 400 sec. Mass Engine: 90 kg (198 lb). Diameter: 1.40 m (4.50 ft). Chambers: 1. Chamber Pressure: 7.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 39.77. Country: USA. First Flight: 1965. Last Flight: 1982. Flown: 57. AJ10-118E used on Rocket Stages Used on stage: Delta E. on launch vehicle: Delta E. Used on stage: Delta E. on launch vehicle: Delta G. Used on stage: Delta E. on launch vehicle: Delta J. Used on stage: Delta E. on launch vehicle: Delta L. Used on stage: Delta E. on launch vehicle: Delta M. Used on stage: Delta E. on launch vehicle: Delta N. Used on stage: Delta E. on launch vehicle: N.                   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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