Maximum thrust
1100 N ±10 N
Thrust specific fuel consumption (TSFC)
<38 g/kN·s
Maximum operating speed
59,000 rpm
COMPACT 1100 N TURBOJET ENGINE FOR MISSILES AND UAVS
The POWERTECH PJ110 is a short-life, expendable turbojet engine designed for missile and UAV applications. Suitable for both air- and ground-launched platforms, the engine is designed and produced in the UAE and is ITAR free.
Engineered for reliable, cost-effective performance, the PJ110 combines flexible mounting and exhaust configurations with advanced inlet optimisation. Optional onboard power generation and POWERTECH engineering support facilitate efficient integration across specific platform requirements.
للمزيد من المعلومات:
KEY FEATURES
- Reliable, cost-effective expendable design
- Suitable for air- and ground-launched platforms
- ITAR free
- Optional onboard power generation
SPECIFICATIONS
- Maximum thrust: 1100 N ±10 N
- Nominal continuous thrust: 1000 N ±10 N
- Thrust specific fuel consumption (TSFC): <38 g/kN·s
- Maximum operating speed: 59,000 rpm
- Maximum exhaust gas temperature (EGT): 750°C
