X60AL-1300
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 January 1945. Superperformance
Thrust (sl): 5.780 kN (1,299 lbf). Thrust (sl): 590 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet