LR87-9

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LR87-9

Part of LR87

Aerojet N2O4/Aerozine-50 rocket engine. Variant of LR-87 used on early versions of Titan III B,C First flight 1966.

AKA: AJ23-136. Date: 1970. Thrust: 956.10 kN (214,940 lbf).

Thrust (sl): 956.100 kN (214,940 lbf). Thrust (sl): 97,500 kgf.

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

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