XLR53AJ-1
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 1949. Superperformance, wing tip mounted, regenerative cooling, pressure fed, 240 sec duration, 1000 lbf thrust each.
Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Propellant Formulation: RFNA/Aniline+Furfural Alcohol.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet