.jpg "PS-90A-76 Turbofan engine © Konstantinos Panitsidis")
In numbers Through the lens Video
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Technical specifications
| DESIGNER | UEC-Aviadvigatel JSC |
| COUNTRY | Russia |
| TYPE |
Turbofan engine
|
| Installed On (aerial means) |
Il-76MD-90, Il-76MD-90A, Il-76MF
|
| Fuel |
-
|
| Oil | - |
| Maximum thrust take-off power rating | 14.000 kgf |
| Specific fuel consumption, take-off power rating | 0,372 kg/kgf*h |
| Maximum thrust, cruise power (H=11.000 m, M=0,8) | 3.200 kgf |
| Specific fuel consumption, cruise power | 0,594 kg/kgf*h |
| Pressure ratio, take-off power rating | 29,5 |
| Bypass ratio, take-off power rating | 4,6 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.575 K |
| Air flow rate, take-off power rating | 451 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | - |
| OVERALL DIMENSIONS | |
| Diameter | 1900 mm |
| Height | - |
| Width | - |
| Length | - |
| WEIGHT | |
| Engine weight | 2800 kg |
| Overhaul operation time | - |
| Specified service life | - |
| Shelf life of preserved engine | - |