XJ40-WE-1
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Wright turbojet engine. Out of production. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Used on Navaho X-10 launch vehicle. First flight 1955.
Thrust (sl): 48.500 kN (10,903 lbf). Thrust (sl): 4,943 kgf. Engine: 850 kg (1,870 lb). Thrust to Weight Ratio: 5.81.
Related
- Family
- Turbojet
- Country
- USA
- Launch Vehicles
- Navaho X-10
- Propellants
- Air/Kerosene
- Stages
- Navaho X-10 stage
- Agency
- Wright