.jpg "AI-24 (A) Turboprop engine © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
| DESIGNER | Ivchenko, ZMKB Progress |
| COUNTRY | Russia, Ukraine |
| TYPE |
Turboprop engine
|
| Installed On (aerial means) |
An-24, An-26, An-30
|
| Fuel | Aviation kerosene, JP-1 |
| Oil | - |
| Propeller shaft power, take-off power rating | 2.550 h.p. |
| Specific fuel consumption, take-off power rating | 0,264 kg/h.p.*h |
| Propeller shaft power, cruise power (H=6.000 m, V=450 km/h) | 1.550 h.p |
| Specific fuel consumption, cruise power | 0,245 kg/h.p.*h |
| Pressure ratio, take-take-off power rating | 6,40 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.150 K |
| Air flow rate, take-off power rating | 13,1 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | 15.100 rpm |
| OVERALL DIMENSIONS | |
| Diameter | - |
| Height | 1075 mm |
| Width | 677 mm |
| Length | 2345 mm |
| WEIGHT | |
| Engine weight | 600 kg |
| Specified service life | ~22.000 h |