|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:armament
|
gptkb:30_mm_2A42_autocannon
air-to-air missiles
rocket pods
anti-tank guided missiles
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:crew
|
1
|
|
gptkbp:developedBy
|
gptkb:Kamov_Ka-52
|
|
gptkbp:displayedAt
|
gptkb:MAKS_Airshow
|
|
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
|
Kamov Ka-50
|
|
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
|
parachute
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
|
|
gptkbp:rotorConfiguration
|
coaxial rotors
|
|
gptkbp:status
|
limited service
|
|
gptkbp:bfsParent
|
gptkb:VK-2500_engine
gptkb:Central_Museum_of_the_Air_Forces_at_Monino
gptkb:Sergei_Mikheev
gptkb:Kamov_Ka-52
gptkb:Progress_Arsenyev_Aviation_Company
gptkb:Kamov
|
|
gptkbp:bfsLayer
|
6
|