PJ40

DEPENDABLE THRUST. DETERMINED PERFORMANCE.

PJ40
Maximum thrust 500 N at sea level, ISA conditions
Engine type Turbojet engine
Weight 6 kg

500 N TURBOJET ENGINE FOR MISSILES AND UAVS

The POWERTECH PJ40 is an ITAR free indigenously designed and manufactured 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, PJ40 is ideal for unmanned aerial vehicles and missile systems.

SPECIFICATIONS

  • Maximum thrust: 500 N at sea level, ISA conditions
  • Length: 390 mm
  • Diameter: 155 mm
  • Weight: 6 kg
  • Maximum continuous thrust: 450 N at sea level, ISA conditions

KEY FEATURES

  • ITAR free
  • Excellent Thrust-to-Weight Ratio
  • Advanced Engineering Support Including Air Inlet Channel Optimization
  • In-House Engine Testing Capabilities