Klimov VK-2500

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The Klimov VK-2500 is a Russian turboshaft aero-engine, a high power derivative of the Klimov ТV7-117VMA engine also for hot and high.

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

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

References

External links

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