.jpg "NK-4 Turboprop engine © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
| DESIGNER | Kuznetsov Design Buream |
| COUNTRY | Russia |
| TYPE |
Turboprop engine
|
| Installed On (aerial means) |
Il-18, An-10
|
| Fuel | - |
| Oil | - |
| Propeller shaft power, take-off power rating | 4.000 h.p. |
| Specific fuel consumption, take-off power rating | 0,245 kg/h.p.*h |
| Propeller shaft power, cruise power (H=8.000 m, M=0,57) | 2.300 h.p. |
| Specific fuel consumption, cruise power | 0,207 kg/h.p.*h |
| Pressure ratio, take-take-off power rating | 7,7 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.170 K |
| Air flow rate, take-off power rating | 18,7 kg/sec |
| OVERALL DIMENSIONSΣ | |
| Diameter | 1050 mm |
| Height | - |
| Width | - |
| Length | 2770 mm |
| WEIGHT | |
| Engine weight | 970 kg |
| Specified service life | - |