| Junkers Jumo 012 ✕ | Honeywell/ITEC F124 ✕ | |
|---|---|---|
| Aircraft Engine Manufacturer | Junkers | Garrett |
| Aircraft Engine Type | Turbojet | Turbofan |
| Dry Weight (kg) | 2000 | 476.272 |
| Diameter (mm) | 1064 | 914.4 |
| Length (mm) | 4860 | 2593.34 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Junkers_Jumo_012 | en.wikipedia.org/wiki/Honeywell/ITEC_F124 |
| Geared Fan | No | No |
| Combustion Chamber | 8 chamber can-type | |
| Afterburner | No | No |
| Streams | 1 | 2 |
| Bypass Ratio | 0.49 | |
| Maximum Takeoff Thrust (kN) | 27.3 | 28 |
| Thrust To Weight | 1.39 | 5.3 |
| Compressor Description | 11-stage axial compressor | 3 axial fan (low pressure compressor) stages, 4 axial high pressure compressor stages, 1 centrifugal high pressure compressor stage |
| Turbine Description | 2-stage | 1 stage high pressure turbine, 1 stage low pressure turbine |