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 Klimov ТV7-117VMA engine.

Contents 1 Design 2 Variants 3 Applications 4 Specifications VK-2500 5 References 6 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-2500-01

Has 1750shp (1287kW) maximum continuous performance and a 2400 shp (1764kW) take-off performance

VK-2500-02

Has a 1500shp (1103kW) maximum continuous performance and a 2200 shp (1617kW) take-off performance

VK-2500-03

Has a 1500shp (1103kW) maximum continuous performance and a 2000 shp (1470kW) take-off performance

Applications

• Kamov Ka-50
• Kamov Ka-52
• Mil Mi-28

Specifications VK-2500

Data from http://www.motorsich.com/eng/products/aircraft/turboshaft/vk-2500

General characteristics

• Type: Turboshaft
• Length:
• Diameter:
• Dry weight: 300kg

Components

• Compressor:

Performance

• Maximum power output: 1287kW (1750shp)
• Specific fuel consumption: 0.22 kg/hp/hr
• Power-to-weight ratio:

References

• [1]

External links

• Manufacturer's website

Klimov aircraft engines Piston engines M-100 · M-103 · M-105 · M-110 · M-120 · VK-106 · VK-107 · VK-108 · VK-109 · VK-110 · VK-150 Turbojets RD-45 · RD-500 Turbofans RD-33 Turboprops and turboshafts TV3-117 · TV7-117 · VK-800 · VK-1500 · VK-2500 · VK-3000

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