| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbojet |
| Dry Weight (kg) |
450 |
314.7931 |
| Diameter (mm) |
970.3 |
619.76 |
| Length (mm) |
2062 |
2781.3 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Pratt_%26_Whitney_Canada_PW300 |
en.wikipedia.org/wiki/General_Electric_J97 |
| Fuel |
Aviation Kerosene such as JET A, JET A-1, JP-4, JP-5 or CPW-204 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular |
annular |
| Afterburner |
No |
Yes |
| Streams |
2 |
1 |
| Bypass Ratio |
4.5 |
|
| Maximum Takeoff Thrust (kN) |
23.24 |
23.4 |
| Thrust To Weight |
5.26 |
11.5 |
| Specific Fuel Consumption (g/(kN·s)) |
11.528 |
|
| Afterburner Thrust (kN) |
|
35 |
| Compressor Description |
1-stage fan, 4-stage axial with 1-stage centrifugal high pressure compressor |
14-stage |
| Turbine Description |
2 stage high pressure, 3 stage low pressure turbines. |
two-stage |