X90ALT-60000
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 April 1947. Unspecified Application, 20,000 lbf subscale tested, new vertical test facility
Thrust (sl): 264.000 kN (59,349 lbf). Thrust (sl): 27,000 kgf. Propellant Formulation: Nitric acid/Aniline+Furfural Alcohol.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet