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25XALD-1000
Part of LR53 engine series Family
Aerojet Nitric acid/Amine JATO rocket engine. Development begun May 1942. Droppable version of XLR1, packaged compactly with parachute, for P-38, B-24, and B-25J. First flight 1944.

AKA: XLR3-AJ-1. Date: May 1942. Thrust: 4.41 kN (991 lbf). Unfuelled mass: 124 kg (273 lb). Burn time: 25 s. Height: 1.75 m (5.74 ft). Diameter: 0.61 m (2.00 ft).

Three spherical propellant tanks, single uncooled thrust chamber, pressure fed.

Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 124 kg (273 lb). Chamber Pressure: 20.00 bar. Propellant Formulation: RFNA/Aniline.

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



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