XLR53AJ-1

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XLR53AJ-1

Part of LR53 engine series

Aerojet Nitric acid/Amine rocket engine. Development begun 1949. Superperformance, wing tip mounted, regenerative cooling, pressure fed, 240 sec duration, 1000 lbf thrust each.

AKA: XLR53-AJ-1. Status: Out of Production. Date: 1949. Thrust: 4.41 kN (991 lbf).

Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.

Family: Storable liquid. Country: USA. Propellants: Nitric acid/Amine. Agency: Aerojet.

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