.jpg "Turbofan engine D-30-II © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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TECHNICAL SPECIFICATIONS
| Fuel | T-1, TS-1 |
| Oil | MK-8, MK-8P |
| Max thrust take-off power rating | 6.930 kgf |
| Specific fuel consumption, take-off power rating | 0,610 kg/kgf.*h |
| Max thrust, cruise power | 1.600 kgf |
| Specific fuel consumption, cruise power | 0,793 kg/kgf.*h |
| Pressure ratio, take-off power rating | 20,2 |
| Bypass ratio | 0,843 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.330 K |
| Air flow rate, take-off power rating | 128 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Compressor rotation frequency high-pressure, take-off power rating | |
| Diameter | - |
| Height | - |
| Width | - |
| Length | - |
| Weight | 1809 kg |
| Specified service life | - |