Maximum continuous thrust
450 N at sea level, ISA conditions
Engine type
Piston
Weight
6 kg
Diameter
155 mm
400 N TURBOJET ENGINE FOR MISSILES AND UAVS
The POWERTECH PJ40 is an ITAR free indigenously designed and manufactured small turbojet engine for missiles and UAVs. The engine has an excellent thrust-to-weight ratio, compact diameter, and efficient fuel consumption.
Operational in all weather conditions and incorporating more than 20 sensors and function redundancies, the PJ40 is ideal for unmanned aerial vehicles with its long service intervals of at least 1,000 hours.
For more details:
SPECIFICATIONS
- Length: 390 mm
- Diameter: 155 mm
- Weight: 6 kg
- Maximum continuous thrust: 450 N at sea level, ISA conditions
- Width: 400 mm | Length: 300 mm
- Height: 240 mm
- Engine type: Piston
- Operating principle: 2-stroke
- Fuelling: Electronic fuel injection
- Oiling: Separate oil injection (integrated oil tank)
