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