| Aircraft Engine Manufacturer |
IHI Corporation |
Pratt & Whitney |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
644 |
2347.341 |
| Diameter (mm) |
610 |
990.6 |
| Length (mm) |
3000 |
6197.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/IHI_Corporation_XF5 |
en.wikipedia.org/wiki/Pratt_%26_Whitney_J57 |
| Geared Fan |
No |
No |
| Combustion Chamber |
annular |
cannular, 8 flame tubes |
| Afterburner |
Yes |
Yes |
| Streams |
2 |
1 |
| Maximum Takeoff Thrust (kN) |
49 |
52 |
| Thrust To Weight |
7.8 |
2.26 |
| Afterburner Thrust (kN) |
49 |
76.5 |
| Compressor Description |
axial, 3 stage fan, 6 compressor stage |
all-axial, 9-stage LP compressor, 7-stage HP compressor |
| Turbine Description |
1 stage high pressure turbine, 1 stage low pressure turbine |
all-axial, single-stage HP turbine, 2-stage LP turbine |