.jpg "D-30KP Turbofan engine © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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TECHNICAL SPECIFICATIONS
| Fuel | T-1, TC-1 |
| Oil | MK-8, MK-8P |
| Max thrust take-off power rating | 12.000 kgf |
| Specific fuel consumption, take-off power rating | 0,5 kg/kgf.*h |
| Max thrust, cruise power (H=11.000 m, M=0,8) | 2.750 kgf |
| Specific fuel consumption, cruise power | 0,7 kg/kgf.*h |
| Pressure ratio, take-off power rating | - |
| Bypass ratio, take-off power rating | 2,36 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.427 K |
| Air flow rate, take-off power rating | 279 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 | 2.640 kg |
| Specified service life | - |
