| Aircraft Engine Manufacturer |
EuroJet |
Volvo Aero |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Dry Weight (kg) |
989 |
1054 |
| Diameter (mm) |
736.6 |
870 |
| Length (mm) |
3987.8 |
4040 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Eurojet_EJ200 |
en.wikipedia.org/wiki/Volvo_RM12 |
| Fuel |
|
MC 75 |
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular |
annular |
| Afterburner |
Yes |
Yes |
| Streams |
2 |
2 |
| Bypass Ratio |
0.4 |
0.31 |
| Maximum Takeoff Thrust (kN) |
60 |
54 |
| Thrust To Weight |
6.11 |
7.8 |
| Specific Fuel Consumption (g/(kN·s)) |
|
676.968 |
| Afterburner Thrust (kN) |
60 |
80.5 |
| Compressor Description |
Axial, 3-stage LP, 5-stage HP |
Axial compressor with 3 fan and 7 compressor stages |
| Turbine Description |
1-stage LP, 1-stage HP |
1 low-pressure, max 221 r/s and 1 high-pressure stage, max 280 r/s |