LR87-11 AJ23-138

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LR87-11 AJ23-138

Part of LR87

Aerojet N2O4/Aerozine-50 rocket engine. Version of LR-87-11 tuned for launch pad ignition when used on Titan 3B. First flight 1966.

AKA: AJ23-138;LR87-11. Date: 1968. Thrust: 1,008.31 kN (226,677 lbf).

Thrust (sl): 1,008.310 kN (226,677 lbf). Thrust (sl): 102,820 kgf.

Family: Storable liquid. Country: USA. Launch Vehicles: Titan IIIB. Propellants: N2O4/Aerozine-50. Agency: Aerojet.

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