gptkbp:instanceOf
|
gptkb:helicopter
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
gptkbp:crew
|
5
|
gptkbp:enginePower
|
4,100 kW each
|
gptkbp:exportedTo
|
gptkb:Algeria
gptkb:Bulgaria
gptkb:China
gptkb:Cuba
gptkb:Czechoslovakia
gptkb:East_Germany
gptkb:Egypt
gptkb:Hungary
gptkb:India
gptkb:Indonesia
gptkb:Iraq
gptkb:North_Korea
gptkb:Peru
gptkb:Poland
gptkb:Romania
gptkb:Syria
gptkb:Vietnam
|
gptkbp:firstFlight
|
1957-09-05
|
gptkbp:height
|
9.86 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi-6
|
gptkbp:introduced
|
1957
|
gptkbp:length
|
33.18 m
|
gptkbp:mainRotorDiameter
|
35 m
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
gptkbp:maximumSpeed
|
300 km/h
|
gptkbp:maxTakeoffWeight
|
42,500 kg
|
gptkbp:NATOReportingName
|
gptkb:Hook
|
gptkbp:numberBuilt
|
926
|
gptkbp:payload
|
12,000 kg
|
gptkbp:powerplant
|
2 × Soloviev D-25V turboshaft engines
|
gptkbp:primaryUser
|
gptkb:Russian_Air_Force
gptkb:Soviet_Air_Force
|
gptkbp:range
|
620 km
|
gptkbp:retired
|
2002
|
gptkbp:role
|
heavy transport helicopter
|
gptkbp:serviceCeiling
|
4,500 m
|
gptkbp:successor
|
gptkb:Mil_Mi-26
|
gptkbp:usedInConflict
|
gptkb:Soviet–Afghan_War
Chernobyl disaster response
|
gptkbp:variant
|
gptkb:Mi-6TZ
gptkb:Mi-6VKP
gptkb:Mi-6A
gptkb:Mi-6PP
gptkb:Mi-6SAR
gptkb:Mi-6VPK
|
gptkbp:bfsParent
|
gptkb:Soviet_Air_Force
|
gptkbp:bfsLayer
|
5
|