AJ10-118F Manufacturer Name: AJ10-118F. Designer: Aerojet. Propellants: Nitric acid/UDMH. Thrust(vac): 41.400 kN (9,307 lbf). Isp: 306 sec. Burn time: 335 sec. Mass Engine: 95 kg (209 lb). Diameter: 1.40 m (4.50 ft). Chambers: 1. Chamber Pressure: 9.00 bar. Area Ratio: 40.00. Thrust to Weight Ratio: 44.40. Country: USA. First Flight: 1972. Last Flight: 1987. Flown: 13. AJ10-118F used on Rocket Stages Used on stage: Delta F. on launch vehicle: Delta 0100. Used on stage: Delta F. on launch vehicle: N-2.                   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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