| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
Garrett |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Dry Weight (kg) |
450 |
510.2914 |
| Diameter (mm) |
970.3 |
853.44 |
| Length (mm) |
2062 |
2590.8 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Pratt_%26_Whitney_Canada_PW300 |
en.wikipedia.org/wiki/Garrett_ATF3 |
| Fuel |
Aviation Kerosene such as JET A, JET A-1, JP-4, JP-5 or CPW-204 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular |
Reverse-flow annular type |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
4.5 |
2.8 |
| Maximum Takeoff Thrust (kN) |
23.24 |
24.2 |
| Thrust To Weight |
5.26 |
|
| Specific Fuel Consumption (g/(kN·s)) |
11.528 |
|
| Compressor Description |
1-stage fan, 4-stage axial with 1-stage centrifugal high pressure compressor |
Single-stage low-pressure fan, five-stage intermediate-pressure axial compressor and single-stage high-pressure centrifugal compressor |
| Turbine Description |
2 stage high pressure, 3 stage low pressure turbines. |
Three-stage: single-stage high-pressure, three-stage intermediate-pressure and two-stage low-pressure |