.jpg "Klimov VK-1 jet 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 | 2.700 kgf |
| Specific fuel consumption, take-off power rating | 1,07 kg/kgf.*h |
| Max thrust, cruise power | - |
| Specific fuel consumption, cruise power | - |
| Pressure ratio, take-off power rating | 4,2 |
| Bypass ratio | - |
| Temperature of the gas at the turbine intake, take-off power rating | 1.170 K |
| 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 | 1270 mm |
| Height | - |
| Width | - |
| Length | 2640 mm |
| Weight | 870 kg |
| Specified service life | - |
