Maximum thrust
1000 N ±10 N
Thrust specific fuel consumption (TSFC)
<38 g/kN·s
Maximum operating speed
63,000 rpm
COMPACT 900 N TURBOJET ENGINE FOR MISSILES AND UAVS
The POWERTECH PJ90 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 cost-effective performance, the PJ90 combines flexible mounting and exhaust configurations with advanced inlet optimisation. POWERTECH also provides engineering support and in-house testing capabilities to facilitate efficient integration across specific platform requirements.
For more details:
KEY FEATURES
- Cost-effective expendable design
- Suitable for air- and ground-launched platforms
- ITAR free
- Flexible mounting and exhaust configurations
SPECIFICATIONS
- Maximum thrust: 1000 N ±10 N
- Nominal continuous thrust: 900 N ±10 N
- Thrust specific fuel consumption (TSFC): <38 g/kN·s
- Maximum operating speed: 63,000 rpm
- Maximum exhaust gas temperature (EGT): 750°C
