| Eurojet EJ200 ✕ | Snecma M53 ✕ | |
|---|---|---|
| Aircraft Engine Manufacturer | EuroJet | SNECMA |
| Aircraft Engine Type | Turbofan | Turbofan |
| Dry Weight (kg) | 989 | 1515 |
| Diameter (mm) | 736.6 | 796 |
| Length (mm) | 3987.8 | 5070 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Eurojet_EJ200 | en.wikipedia.org/wiki/Snecma_M53 |
| Geared Fan | No | No |
| Combustion Chamber | Annular | annular |
| Afterburner | Yes | Yes |
| Streams | 2 | 2 |
| Bypass Ratio | 0.4 | 0.36 |
| Maximum Takeoff Thrust (kN) | 60 | 64 |
| Thrust To Weight | 6.11 | 6.5 |
| Specific Fuel Consumption (g/(kN·s)) | 25.492 | |
| Afterburner Thrust (kN) | 60 | |
| Compressor Description | Axial, 3-stage LP, 5-stage HP | 8-stage axial compressor |
| Turbine Description | 1-stage LP, 1-stage HP | 2-stage axial turbine |