Acid-Aniline 4000 lbf thrust
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 December 1946. Engine design and testing
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