VK-1500VK
The VK-1500VK engine is a turboshaft version of the VK-1500
engine. The engine can be used as powerplant for mediumclass
helicopters Ka-62.
High level of designing and production capabilities gave
the oportunity to create the engine, that features high
performance, reliability and long service life.
The engine complies with the requirements of Aviation
Rules AP-33.
Main advantages:
- High economy;
- Reliability and trouble-free operation;
- The engine is controlled by combined electro-hydraulic control and monitoring system featuring full electronic authority;
- Levels of pollutant emission and exhaust opacity are lower than those required by ICAO Standards;
- Low noise level;
- In-service repair.
Basic specifications:
| Takeoff power condition (Н=О, Мfl=О, ISA+20°C): | |
| Power, shp (kW) | 1600 (1176) |
| Specific fuel consumption, kg/hp.h (kg/kW·h) | 0.240 (0.326) |
| Emergency power condition (Н=О, Мfl=О, ISA): | |
| Power, shp (kW) | 1800-1900 |
| Cruise power condition (Н=О, Мfl=О, ISA+25°C): | |
| Power, shp (kW) | 1100 (809) |
| Specific fuel consumption, kg/hp·h (kg/kW·h) | 0.265 (0.360) |
| Dry weight, kg | 250...270 |
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