25XALD-1000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Amine JATO rocket engine. Development begun May 1942. Droppable version of XLR1, packaged compactly with parachute, for P-38, B-24, and B-25J. First flight 1944.
Three spherical propellant tanks, single uncooled thrust chamber, pressure fed.
Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 124 kg (273 lb). Chamber Pressure: 20.00 bar. Propellant Formulation: RFNA/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet