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