| Aircraft Engine Manufacturer |
Hindustan Aeronautics Limited |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
350 |
314.7931 |
| Diameter (mm) |
590 |
619.76 |
| Length (mm) |
1730 |
2781.3 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/HAL_HTFE-25 |
en.wikipedia.org/wiki/General_Electric_J97 |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
annular |
| Afterburner |
No |
Yes |
| Streams |
2 |
1 |
| Bypass Ratio |
0.5 |
|
| Maximum Takeoff Thrust (kN) |
25 |
23.4 |
| Thrust To Weight |
7.27 |
11.5 |
| Afterburner Thrust (kN) |
|
35 |
| Compressor Description |
|
14-stage |
| Turbine Description |
|
two-stage |