D-136/D-136, Series 1
It is used for heavy helicopters. The maximum takeoff power is 11,400 hp.
Quality and reliability of the engine are ensured by perfect design and high degree of maturity of mass production process.
Easy maintenance and high repairability are ensured by the engine modular design. |
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Main advantages of the engine:
- Low specific fuel consumption;
- High reliability;
- High power;
- Easy maintenance and high repairability;
- Low weight-to-power ratio.
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Basic specifications:
| Maximum takeoff power rating (SLS, ISA) |
| Power, shp (kW) |
11,400 (8,382) |
| Specific fuel consumption, kg/hp•h (kg/kW•h) |
0.194 (0.263) |
| Cruise power rating (H=4,600 m, M=0,13; ISA) |
| Power, shp (kW) |
6,100 (4,486) |
| Specific fuel consumption, kg/hp•h (kg/kW•h) |
0.230 (0.312) |
| Dry weight, kg |
1,077 |
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