.jpg "Turboshaft engine TV3-117VMA-SBM1V © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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Designers: Motor Sich, JSC Zaporozhye, Ukraine
Manufacturer: Motor Sich, JSC Zaporozhye, Ukraine
This engine is intended for new helicopters and for retrofitting the in-service helicopters.
TECHNICAL SPECIFICATIONS
| Fuel | - |
| Oil | - |
| Propeller shaft power, take-off power rating | 2.500 h.p. |
| Specific fuel consumption, take-off power rating | 0,199 kg/e.h.p.*h |
| Propeller shaft power, cruise power (H=6.000 m, V=500 km/h) | 1.750 h.p. |
| Specific fuel consumption, cruise power | 0,188 kg/e.h.p.*h |
| Pressure ratio, take-take-off power rating | 10 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.293 K |
| Air flow rate, take-off power rating | 9,3 kg/sec |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Diameter | - |
| Height | 1210 mm |
| Width | 880 mm |
| Lenght | 2860 mm |
| Weight | 570 kg |
| Specified service life | - |
