Acid-Aniline 4000 lbf thrust

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Acid-Aniline 4000 lbf thrust

Part of 40AL

Aerojet Nitric acid/Amine rocket engine. Development begun December 1946. Engine design and testing

AKA: Acid/Aniline 4000 lbf thrust. Date: December 1946. Thrust: 17.60 kN (3,957 lbf).

Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Propellant Formulation: Nitric acid/Aniline.

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

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