| Aircraft Engine Manufacturer |
Williams International |
Teledyne CAE |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
30.3907 |
46.0396 |
| Diameter (mm) |
304.8 |
317.5 |
| Length (mm) |
609.6 |
736.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Williams_F107 |
en.wikipedia.org/wiki/Teledyne_CAE_J402 |
| Fuel |
JP-4 / JP-5 / JP-10 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular combustion chamber |
Annular |
| Afterburner |
No |
No |
| Streams |
2 |
1 |
| Bypass Ratio |
1 |
|
| Maximum Takeoff Thrust (kN) |
2.7 |
2.9 |
| Thrust To Weight |
6.42 |
6.5 |
| Specific Fuel Consumption (g/(kN·s)) |
19.346 |
|
| Compressor Description |
2-stage fan, 2-stage axial IP compressor, 1-stage centrifugal HP compressor |
Single stage axial compressor, single stage centrifugal compressor |
| Turbine Description |
1-stage HP turbine, 2-stage LP turbine |
Single stage high pressure turbine |