HJD-X ENGINE

High Performance Turbojet Engine

HJD-X ENGINE

The HJD-X engine family consists of three high performance short life turbojet engines designed specifically for missile applications. The family consists of the HJD-X40, HJD-X75 and the HJD-X100, which have been developed using state-of-the-art design and performance modelling software and world-class manufacturing processes.

 

 

HJD-X 40daN

HJD-X 75daN

HJD-X 100daN

Nominal Thrust at sea-level:

400 N 

750 N

1,000 N

Maximum Operating Altitude: 

10,000m

10,000m

10,000m

Maximum Start-up Altitude at Mach 0.4 or higher:

6,000m

6,000m

6,000m

Maximum flight speed:

Mach 0.85

Mach 0.85 

Mach 0.85

Endurance:

60 minutes

60 minutes

60 minutes

Max Engine Speed:

87,000RPM

63,500RPM

55,500RPM