|
gptkbp:instanceOf
|
gptkb:helicopter
|
|
gptkbp:avionics
|
KRET avionics suite
|
|
gptkbp:capacity
|
30 passengers
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruiseSpeed
|
285 km/h
|
|
gptkbp:enginePower
|
2,800 hp each
|
|
gptkbp:enteredService
|
2019
|
|
gptkbp:firstFlight
|
2003-12-22
|
|
gptkbp:firstPrototype
|
1994
|
|
gptkbp:fuelType
|
3,320 kg
|
|
gptkbp:hasVariant
|
Mi-38-2
Mi-38T
|
|
gptkbp:height
|
5.13 m
|
|
gptkbp:landingGear
|
fixed tricycle landing gear
|
|
gptkbp:length
|
19.95 m
|
|
gptkbp:mainRotorDiameter
|
21.1 m
|
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:maximumSpeed
|
300 km/h
|
|
gptkbp:maxTakeoffWeight
|
15,600 kg
|
|
gptkbp:NATOReportingName
|
gptkb:Havoc
|
|
gptkbp:numberBuilt
|
over 20
|
|
gptkbp:operator
|
gptkb:Russian_Air_Force
gptkb:Russian_Helicopters
gptkb:Russian_Ministry_of_Emergency_Situations
|
|
gptkbp:powerplant
|
2 × Klimov TV7-117V turboshaft engines
|
|
gptkbp:range
|
1,200 km
|
|
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
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mil Mi-38
|