| Ivchenko AI-24 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Ivchenko-Progress ZMKB |
| Aircraft Engine Type | Turbopropulsor |
| Dry Weight (kg) | 600 |
| Diameter (mm) | 360 |
| Length (mm) | 2436 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Ivchenko_AI-24 |
| Fuel | Aviation Kerosene / JP-1 or similar |
| Combustion Chamber | Annular combustion chamber with 8 flame tubes |
| Maximum Takeoff Power (kW) | 2087.96 |
| Specific Fuel Consumption (g/(kW·h)) | 324.2 |
| Compressor Description | 10-stage axial |
| Turbine Description | 3-stage axial |