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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
gptkb:30_mm_Shipunov_2A42_autocannon
rockets
air-to-air missiles
anti-tank guided missiles
|
|
gptkbp:avionics
|
gptkb:laser
gptkb:radar
night vision system
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:crew
|
1
|
|
gptkbp:developedBy
|
gptkb:Kamov_V-80
|
|
gptkbp:ejectionSystem
|
gptkb:K-37-800_ejection_seat
|
|
gptkbp:emptyWeight
|
7,700 kg
|
|
gptkbp:engine
|
gptkb:Klimov_VK-2500
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:height
|
4.93 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ka-50 Black Shark
|
|
gptkbp:introduced
|
1995
|
|
gptkbp:length
|
16.0 m
|
|
gptkbp:manufacturer
|
gptkb:Kamov
|
|
gptkbp:maximumSpeed
|
310 km/h
|
|
gptkbp:maxTakeoffWeight
|
10,800 kg
|
|
gptkbp:NATOReportingName
|
gptkb:Hokum_A
|
|
gptkbp:nickname
|
gptkb:Black_Shark
|
|
gptkbp:notableFeature
|
coaxial rotor system
single-seat design
|
|
gptkbp:numberOfEngines
|
2
|
|
gptkbp:primaryUser
|
gptkb:Russian_Air_Force
|
|
gptkbp:range
|
545 km
|
|
gptkbp:role
|
close air support
anti-armor operations
|
|
gptkbp:rotorConfiguration
|
coaxial rotors
|
|
gptkbp:status
|
limited service
|
|
gptkbp:usedInConflict
|
gptkb:Syrian_Civil_War
gptkb:Second_Chechen_War
|
|
gptkbp:variant
|
gptkb:Ka-52_Alligator
|
|
gptkbp:bfsParent
|
gptkb:Digital_Combat_Simulator
gptkb:DCS_World
|
|
gptkbp:bfsLayer
|
7
|