|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:accessories
|
fuel control unit
|
|
gptkbp:application
|
gptkb:helicopter
|
|
gptkbp:average_temperature
|
up to 1500 ° C
-50 to +50 ° C
|
|
gptkbp:certification
|
certified by Russian authorities
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:commissioned
|
2000s
|
|
gptkbp:competitors
|
gptkb:Pratt_&_Whitney_PT6
gptkb:General_Electric_T700
gptkb:Rolls-Royce_M250
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:configuration
|
two-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
1990s
derived from TV3-117 engine
|
|
gptkbp:emissions_standard
|
meets ICAO standards
|
|
gptkbp:environmental_impact
|
low environmental impact
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_economy
|
high fuel efficiency
low fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
VK-2500 engine
|
|
gptkbp:investment
|
high pressure
|
|
gptkbp:launch_date
|
less than 30 seconds
|
|
gptkbp:launch_window
|
starter-generator
|
|
gptkbp:maintenance
|
1000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:market
|
military aviation market
|
|
gptkbp:noise_level
|
low noise level
low vibration level
|
|
gptkbp:notable_users
|
gptkb:Egyptian_Air_Force
gptkb:Indian_Armed_Forces
gptkb:Russian_Armed_Forces
gptkb:Azerbaijan_Air_Force
gptkb:Kazakhstan_Air_Force
|
|
gptkbp:power_output
|
2400 hp
|
|
gptkbp:propulsion
|
8 hp/kg
up to 2700 kgf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service
|
up to 4000 hours
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:used_in
|
gptkb:Kamov_Ka-52
gptkb:Mil_Mi-28
|
|
gptkbp:variant
|
gptkb:VK-2500_M
gptkb:VK-2500_V
VK-2500 P
|
|
gptkbp:weight
|
about 300 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|