Aerojet N2O4/Aerozine-50 rocket engine. Launch thrust 1008.31 kN. Version of LR-87-11 tuned for launch pad ignition when used on Titan 3B. First flight 1966.
Thrust (sl): 1,008.310 kN (226,677 lbf). Thrust (sl): 102,820 kgf.
More... - Chronology...
Thrust: 1,008.31 kN (226,677 lbf).
First Launch: 1968.
Associated Launch Vehicles
Titan 3B American orbital launch vehicle. Titan core with Agena upper stage. Found to be more cost effective and higher performance than using Transtage. More...
Associated Manufacturers and Agencies
Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
N2O4/Aerozine-50 Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Aerozine was a 50-50 mixture of hydrazine and UDMH developed for use in the Titan 2 missile. Copied in one Russian missile but otherwise straight UDMH used more commonly. Higher boiling point than UDMH. More...
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