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XLR13-AJ-5
Part of LR13 Family
Aerojet Nitric acid/Amine rocket engine. Development begun June 1948. Ceramic chamber and nozzle, nitrogen pressure-fed, droppable but no recoverable.

AKA: X45ALD-4000. Date: June 1948. Thrust: 17.60 kN (3,957 lbf). Burn time: 60 s.

Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Propellant Formulation: RFNA/70% Xylidine+30% AN-F-48.



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

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