40XAL-4000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Amine rocket engine. Development begun July 1943. Gasoline engine driven pumps. Also 40ALD-6000 and 60ALD-8000 versions First flight 1945.
Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Propellant Formulation: Nitric acid/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet