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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:accessories
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gptkb:Twix
gptkb:spark_plug
gptkb:oil_and_gas_industry
gptkb:Control_Panel
gptkb:sensors
gptkb:exhaust_system
temperature sensors
fuel pumps
wiring harness
oil cooler
mounting brackets
cooling fan
fuel filter
starter motor
control valves
fuel control unit
vibration monitoring system
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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:certification
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Russian certification
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gptkbp:combustor_type
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annular
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gptkbp:competitors
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gptkb:General_Electric_T700
gptkb:Rolls-Royce_M250
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gptkbp:compression_ratio
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16:1
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gptkbp:control_system
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digital electronic control
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gptkbp:cooling_system
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air-cooled
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gptkbp:design_feature
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modular design
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gptkbp:development
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gptkb:Soviet_Union
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gptkbp:diameter
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0.5 m
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gptkbp:emissions_standard
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low
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gptkbp:engine
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gptkb:Klimov_TV3-117
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gptkbp:engine_configuration
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flexible mount
twin-shaft
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gptkbp:exhaust_system
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gptkb:single
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gptkbp:first_flight
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gptkb:1996
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gptkbp:fuel_economy
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high
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gptkbp:fuel_type
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gptkb:Jet_A-1
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|
https://www.w3.org/2000/01/rdf-schema#label
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Klimov VK-2500
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gptkbp:length
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1.5 m
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gptkbp:maintenance
|
200 hours
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gptkbp:manufacturer
|
Klimov
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gptkbp:market
|
global
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gptkbp:noise_level
|
low
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gptkbp:operational_history
|
1996-present
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gptkbp:power_output
|
1864 k W
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gptkbp:propulsion
|
2500 hp
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gptkbp:successor
|
Klimov VK-2500 P
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gptkbp:type
|
starter-generator
turbo-shaft
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gptkbp:used_in
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gptkb:Mil_Mi-24
gptkb:Kamov_Ka-50
gptkb:Mil_Mi-28
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gptkbp:weight
|
300 kg
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gptkbp:bfsParent
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gptkb:Kamov_Ka-50
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gptkbp:bfsLayer
|
6
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