LR91-9 (original) (raw)

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LR91-9

Part of LR91

Aerojet N2O4/Aerozine-50 rocket engine. Titan III B, C, D. Out of Production. Version used in earlier versions of Titan 3 upper stages. First flight 1965.

AKA: AJ23-137. Status: Out of Production. Date: 1968. Thrust: 448.61 kN (100,850 lbf). Specific impulse: 316 s.

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

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