.jpg "Turbofan engine D-90A (PS-90A) © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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TECHNICAL SPECIFICATIONS
| Fuel | - |
| Oil | - |
| Max thrust take-off power rating | 16.000 kgf |
| Specific fuel consumption, take-off power rating | - |
| Max thrust, cruise power | 3.500 kgf (H=11.000 m, V=850 km/h) |
| Specific fuel consumption, cruise power | 0,595 kg/kgf. h |
| Pressure ratio, take-off power rating | 35,5 |
| Bypass ratio | 4,36 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.565 K |
| Air flow rate, take-off power rating | 470 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | |
| Diameter | 1.900 mm |
| Height | - |
| Width | - |
| Length | 5333 mm |
| Weight | 2950 kg |
| Specified service life | 30.000 h |
