| Aircraft Engine Manufacturer |
Teledyne CAE |
Williams International |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Dry Weight (kg) |
|
30.3907 |
| Diameter (mm) |
|
304.8 |
| Length (mm) |
|
609.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Teledyne_CAE_F106 |
en.wikipedia.org/wiki/Williams_F107 |
| Fuel |
|
JP-4 / JP-5 / JP-10 |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
Annular combustion chamber |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
|
1 |
| Maximum Takeoff Thrust (kN) |
2.7 |
2.7 |
| Thrust To Weight |
|
6.42 |
| Specific Fuel Consumption (g/(kN·s)) |
|
19.346 |
| Compressor Description |
|
2-stage fan, 2-stage axial IP compressor, 1-stage centrifugal HP compressor |
| Turbine Description |
|
1-stage HP turbine, 2-stage LP turbine |