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gptkbp:instanceOf
|
gptkb:helicopter
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gptkbp:avionics
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KRET avionics suite
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|
gptkbp:capacity
|
30 passengers
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gptkbp:countryOfOrigin
|
gptkb:Russia
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|
gptkbp:crew
|
2
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|
gptkbp:cruiseSpeed
|
285 km/h
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|
gptkbp:enginePower
|
2,800 hp each
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gptkbp:enteredService
|
2019
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gptkbp:firstFlight
|
2003-12-22
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|
gptkbp:firstPrototype
|
1994
|
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gptkbp:fuelType
|
3,320 kg
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|
gptkbp:hasVariant
|
Mi-38-2
Mi-38T
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gptkbp:height
|
5.13 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-38
|
|
gptkbp:landingGear
|
fixed tricycle landing gear
|
|
gptkbp:length
|
19.95 m
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gptkbp:mainRotorDiameter
|
21.1 m
|
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gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:maximumSpeed
|
300 km/h
|
|
gptkbp:maxTakeoffWeight
|
15,600 kg
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|
gptkbp:NATOReportingName
|
gptkb:Havoc
|
|
gptkbp:numberBuilt
|
over 20
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|
gptkbp:operator
|
gptkb:Russian_Air_Force
gptkb:Russian_Helicopters
gptkb:Russian_Ministry_of_Emergency_Situations
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gptkbp:powerplant
|
2 × Klimov TV7-117V turboshaft engines
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gptkbp:range
|
1,200 km
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gptkbp:role
|
gptkb:helicopter
transport helicopter
|
|
gptkbp:serviceCeiling
|
5,900 m
|
|
gptkbp:successor
|
gptkb:Mil_Mi-8
|
|
gptkbp:tailRotorType
|
conventional tail rotor
|
|
gptkbp:usedFor
|
search and rescue
cargo transport
passenger transport
medical evacuation
offshore operations
|
|
gptkbp:bfsParent
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:bfsLayer
|
6
|