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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:helicopter
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gptkbp:average_temperature
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-40 to +50 ° C
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gptkbp:combustor_type
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annular combustion chamber
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gptkbp:competitors
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gptkb:General_Electric_T700
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gptkbp:compression_ratio
|
16:1
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gptkbp:compressor_type
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gptkb:3
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gptkbp:control_system
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gptkb:FADEC
digital control system
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gptkbp:cooling_system
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gptkb:oil
air-cooled
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gptkbp:design
|
twin-shaft
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gptkbp:development
|
derived from VK-2500
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gptkbp:elevation
|
up to 6000 m
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gptkbp:emissions_standard
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gptkb:Euro_I
|
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gptkbp:engine_configuration
|
free turbine
|
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gptkbp:engine_type
|
turbo-shaft
|
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gptkbp:first_flight
|
gptkb:2000
|
|
gptkbp:fuel_capacity
|
0.5 m
1.5 m
300 kg
|
|
gptkbp:fuel_economy
|
high efficiency
200 kg/h
|
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gptkbp:fuel_type
|
gptkb:Jet_A-1
|
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gptkbp:history
|
developed in the 1990s
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|
https://www.w3.org/2000/01/rdf-schema#label
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VK-2500 M
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gptkbp:installation
|
helicopter airframe
|
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gptkbp:launch_window
|
electric starter
|
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gptkbp:maintenance
|
1000 hours
|
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gptkbp:manufacturer
|
Klimov
|
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gptkbp:market
|
global market
|
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gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_features
|
high reliability
|
|
gptkbp:operational_use
|
combat missions
|
|
gptkbp:performance
|
excellent performance
|
|
gptkbp:power_output
|
2400 hp
|
|
gptkbp:propulsion
|
8:1
2400 lbf
|
|
gptkbp:reduction_gear
|
planetary gear
|
|
gptkbp:regulatory_compliance
|
certified by EASA
|
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gptkbp:related_aircraft
|
multi-role helicopters
|
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gptkbp:service
|
3000 hours
|
|
gptkbp:successor
|
VK-2500 P
|
|
gptkbp:turbine_type
|
2
nickel alloy
|
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gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Kamov_Ka-52
gptkb:Mil_Mi-28
|
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gptkbp:weight
|
300 kg
|
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gptkbp:bfsParent
|
gptkb:VK-2500_engine
|
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gptkbp:bfsLayer
|
8
|