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XLR13-AJ-7
Part of LR13 Family
Aerojet Nitric acid/Amine rocket engine. Modification of -AJ-1. Regeneratively cooled by fuel, droppable.

AKA: X60ALD-4000. Date: 1948. Thrust: 17.60 kN (3,957 lbf). Burn time: 60 s. Height: 3.43 m (11.25 ft). Diameter: 0.81 m (2.65 ft).

Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Engine: 363 kg (800 lb). Chamber Pressure: 21.00 bar. Propellant Formulation: RFNA/80% Aniline+20%Furfuryl alcohol.



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

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