| Aircraft Engine Manufacturer |
Ivchenko-Progress ZMKB |
| Aircraft Engine Type |
Open-rotor |
| Dry Weight (kg) |
1650 |
| Diameter (mm) |
970 |
| Length (mm) |
4205 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Progress_D-27 |
| Geared Fan |
Yes |
| Combustion Chamber |
Annular combustion chamber |
| Afterburner |
No |
| Streams |
1 |
| Maximum Takeoff Thrust (kN) |
119 |
| Compressor Description |
5-stage axial flow low-pressure compressor (LPC); high-pressure compressor (HPC) with 2 axial stages and 1 centrifugal stage |
| Turbine Description |
1-stage high-pressure turbine (HPT), 1-stage low-pressure turbine (LPT), 4-stage free power turbine |