.jpg "D-30KP-3 \"Burlak\" Turbofan engine © 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 | 13.000 kgf |
| Specific fuel consumption, take-off power rating | 0,404 kg/kgf. h |
| Max thrust, cruise power | 2.800 kgf (H=11.000 m, M=0,8) |
| Specific fuel consumption, cruise power | 0,645 kg/kgf. h |
| Pressure ratio, take-off power rating | - |
| Bypass ratio, take-off power rating | - |
| Temperature of the gas at the turbine intake, take-off power rating | - |
| Air flow rate, take-off power rating | - |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | - |
| Diameter | 1775 mm |
| Height | 1670 mm |
| Width | - |
| Length | 5734 mm |
| Weight | ~2.700 kg |
| Specified service life | - |
