40ALD-3000

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40ALD-3000

Part of 40AL

Aerojet Nitric acid/Amine rocket engine. Development begun October 1943. Droppable version, pressure fed, regeneratively cooled, supplied with 331 kg of propellant. First flight 1945.

AKA: XLR5-AJ-1. Date: October 1943. Thrust: 13.33 kN (2,997 lbf). Unfuelled mass: 450 kg (990 lb). Burn time: 40 s. Height: 3.20 m (10.40 ft). Diameter: 0.81 m (2.65 ft).

Thrust (sl): 13.330 kN (2,997 lbf). Thrust (sl): 1,360 kgf. Engine: 450 kg (990 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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