Klimov VK-2500
The Klimov VK-2500 is a Russian turboshaft aero engine, a high power derivative of the ТV3-117VMA 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
Applications
Kamov Ka-50
Kamov Ka-52
Mil Mi-28
Specifications
Data from Motor Sich , JSC "Klimov"
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
List of aircraft engines
References
Klimov VK-2500
External links
Klimov VK-2500