X4-AL-1000
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Amine rocket engine. Braking rocket for glider. Single uncooled chamber, pressure fed, 13 kg of propellant.
Thrust (sl): 4.410 kN (991 lbf). Thrust (sl): 450 kgf. Engine: 367 kg (809 lb). Chamber Pressure: 18.70 bar. Propellant Formulation: RFNA/Aniline.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet