| Eurojet EJ200 ✕ | Lyulka AL-7 ✕ | |
|---|---|---|
| Aircraft Engine Manufacturer | EuroJet | Lyulka-Saturn |
| Aircraft Engine Type | Turbofan | Turbojet |
| Dry Weight (kg) | 989 | 2010 |
| Diameter (mm) | 736.6 | 1300 |
| Length (mm) | 3987.8 | 6650 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Eurojet_EJ200 | en.wikipedia.org/wiki/Lyulka_AL-7 |
| Geared Fan | No | No |
| Combustion Chamber | Annular | Annular |
| Afterburner | Yes | Yes |
| Streams | 2 | 1 |
| Bypass Ratio | 0.4 | |
| Maximum Takeoff Thrust (kN) | 60 | 67.1 |
| Thrust To Weight | 6.11 | 3.4 |
| Afterburner Thrust (kN) | 60 | |
| Compressor Description | Axial, 3-stage LP, 5-stage HP | Single-spool turbojet 9-stage axial compressor |
| Turbine Description | 1-stage LP, 1-stage HP | 2-stage axial |