Klimov VK-2500
| VK-2500 | |
|---|---|
 | |
| Type | Turboshaft |
National origin | Russia |
| Manufacturer | Klimov |
Major applications | Kamov Ka-50 Kamov Ka-52 Mil Mi-28 |
The Klimov VK-2500 is a Russian turboshaft aero engine, a high power derivative of the TV3-117VMA engine, also for hot and high.[1]
Contents
1 Design
2 Variants
3 Applications
4 Specifications
4.1 General characteristics
4.2 Components
4.3 Performance
5 See also
6 References
7 External links
Design
It differs from the older versions in having an extended overhaul period of the engine hot components, extra gas-dynamic stability at varying duties, engine parameters accuracy and engine control quality, enhanced monitoring depth providing operation of the engine according to its technical condition and better weight characteristics and overall dimensions.
Variants
- VK-2500-I
- Has a 1,500 shp (1,103 kW) maximum continuous performance and a 2,000 shp (1,470 kW) take-off performance.
- VK-2500-II
- Has a 1,500 shp (1,103 kW) maximum continuous performance and a 2,200 shp (1,617 kW) take-off performance.
- VK-2500-III
- Has 1,750 shp (1,287 kW) maximum continuous performance and a 2,400 shp (1,764 kW) take-off performance.
Applications
- Kamov Ka-50
- Kamov Ka-52
Mil Mi-28, Mi-171A2
MI-17V5
Specifications
Data from producers[2][3]
General characteristics
Type: Turboshaft
Length: 2,055 mm
Diameter: 728 mm (height)
Dry weight: 300 kg
Components
Compressor: Axial
Performance
Maximum power output: 1,985 kW (2,700 shp) APR
Specific fuel consumption: 0.21-0.22 kg/hp/hr
Power-to-weight ratio: 8-9 shp/kg
See also
Related lists
- List of aircraft engines
References
^ Klimov VK-2500
^ Motor Sich
^ JSC "Klimov"
External links
 | Wikimedia Commons has media related to Klimov VK-2500. |
- Klimov VK-2500
 | This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
