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gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:capacity
|
40,000 kg
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:crew
|
6
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|
gptkbp:engine
|
gptkb:Soloviev_D-25VF
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:features
|
twin transverse rotors
|
|
gptkbp:firstFlight
|
1968
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|
gptkbp:height
|
12.5 m
|
|
gptkbp:intendedUse
|
transporting heavy and oversized loads for military and civil purposes
|
|
gptkbp:length
|
37 m
|
|
gptkbp:location
|
gptkb:Central_Air_Force_Museum,_Monino,_Russia
|
|
gptkbp:mainRotorDiameter
|
35 m
|
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:maximumSpeed
|
260 km/h
|
|
gptkbp:maxTakeoffWeight
|
105,000 kg
|
|
gptkbp:NATOReportingName
|
gptkb:Homer
|
|
gptkbp:numberBuilt
|
2
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:powerplant
|
4 × 6,500 kW (8,500 shp) Soloviev D-25VF turboshaft engines
|
|
gptkbp:projectCancelled
|
1974
|
|
gptkbp:range
|
500 km
|
|
gptkbp:role
|
heavy-lift cargo helicopter
|
|
gptkbp:setWorldRecord
|
heaviest helicopter ever built
lifted 44,205 kg to 2,255 m altitude in 1969
|
|
gptkbp:status
|
gptkb:prototype
|
|
gptkbp:tailConfiguration
|
conventional tailplane
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_Mil
|
|
gptkbp:bfsLayer
|
7
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-12
|