38ALDW-1500

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38ALDW-1500

Part of 40AL

Aerojet Nitric acid/Amine rocket engine. Development begun July 1943. Regeneratively cooled. Also a few 45ALDW-1500 were built. Droppable version. First flight 1945.

Date: July 1943. Thrust: 6.66 kN (1,497 lbf).

Thrust (sl): 6.660 kN (1,497 lbf). Thrust (sl): 680 kgf. Propellant Formulation: Nitric acid/Aniline.

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

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