Aerojet N2O4/Aerozine-50 rocket engine. Launch thrust 956.1 kN. Variant of LR-87 used on early versions of Titan III B,C First flight 1966.
Thrust (sl): 956.100 kN (214,940 lbf). Thrust (sl): 97,500 kgf.
Thrust: 956.10 kN (214,940 lbf).
More... - Chronology...
First Launch: 1970.
Associated Launch Vehicles
Titan 3C American orbital launch vehicle. Titan 3A with five segment solid motors. Man-rated design originally developed for Dynasoar spaceplane. More...
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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