DG Propulsion

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DG J60

The DG J60 turbojet engine is designed for unmanned aerial vehicles and defense purposes. With a thrust capacity of up to 60 kgf, it stands as the most potent engine within the DG propulsion jet engine lineup.

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Key Features

 
  • Compact structure
  • Impressive thrust-to-weight ratio
  • Customizable to meet customer requirements (hinge adjustments, nozzle length, water-landing capability)
  • Commercial, industrial, and military drone/UAV manufacturers
 
 
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Specifications

 

  • Engine type:- Turbojet

  • Outer diameter:- 207mm

  • Full length:- 600mm

  • Weight:- 11 000g

  • Thrust:- 588N/+60kg @ 100%RPM

  • Max Rpm:- 74 000

  • Idle Rpm:- 22 000

  • Pressure ratio:- 3.5

  • EGT Normally:- 450-720°C

  • Fuel consumption:- 2200ml/min @ 100%

  • Oil consumption:- 4-5%

  • Mixed with fuel:-
    Acceptable fuel types Jet A1, Kerosene and Diesel

  • Oil Aero Shell:- 500, 4% or 2-stroke oil synthetic TCV3

  • Max altitude :-8000m/26 246ft

  • Max speed:-Mach 0,8/1 000km/h

  • Start system:- Direct Kerosene

  • Service interval:- 30 – 45h

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