25AL-1000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Amine rocket engine for A-20 ATO. Development begun May 1942. Production version of GALCIT unit. First flight 1944.
Three spherical propellant tanks, fixed installation, single uncooled thrust chamber, pressure fed, permanent installed in tail cone of engine nacelle.
Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 109 kg (240 lb). Chamber Pressure: 20.00 bar. Propellant Formulation: RFNA/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet