40ALD-3000
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 October 1943. Droppable version, pressure fed, regeneratively cooled, supplied with 331 kg of propellant. First flight 1945.
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.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet