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.
For more details:
|
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 |