XLR13-AJ-5
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 June 1948. Ceramic chamber and nozzle, nitrogen pressure-fed, droppable but no recoverable.
Thrust (sl): 17.600 kN (3,957 lbf). Thrust (sl): 1,800 kgf. Propellant Formulation: RFNA/70% Xylidine+30% AN-F-48.
Related
- Family
- Storable liquid
- Country
- USA
- Propellants
- Nitric acid/Amine
- Agency
- Aerojet