.jpg "Kuznetsov NK-86 Turbofan engine © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
| DESIGNER | Kuznetsov Design Buream |
| COUNTRY | Russia |
| TYPE |
Turbofan engine
|
| Installed On (aerial means) |
Il-86
|
| Fuel | - |
| Oil | - |
| Maximum thrust take-off power rating | 13.000 kgf |
| Specific fuel consumption, take-off power rating | 0,520 kg/kgf*h |
| Maximum thrust, cruise power (H=11.000 m, M=0,8) | 3.220 kgf |
| Specific fuel consumption, cruise power | 0,739 kg/kgf*h |
| Pressure ratio, take-off power rating | 12,93 |
| Bypass ratio, take-off power rating | 1,18 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.172 K |
| Air flow rate, take-off power rating | 288 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | - |
| OVERALL DIMENSIONS | |
| Diameter | 1455 mm |
| Height | - |
| Width | - |
| Length | 5278 mm |
| WEIGHT | |
| Engine weight | 2.750 kg |
| Specified service life | 18.000 h |