XLR24AJ-2
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet Nitric acid/Gasoline rocket engine. Development begun January 1946. Blast turbine, 2500 lbf fixed thrust (both were part of overall R&D contract)
Thrust (sl): 10.700 kN (2,405 lbf). Thrust (sl): 1,100 kgf. Propellant Formulation: WFNA/Gasoline.
Related
- Family
- Storable liquid
- Country
- USA
- Launch Vehicles
- Lark
- Propellants
- Nitric acid/Gasoline
- Agency
- Aerojet