Mil Mi-10

E637968

The Mil Mi-10 is a Soviet heavy-lift transport helicopter, derived from the Mi-6, notable for its long, spindly landing gear and ability to carry large external loads such as vehicles and prefabricated structures.

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All labels observed (1)

Label Occurrences
Mil Mi-10 canonical 2

Statements (48)

Predicate Object
instanceOf Soviet aircraft
heavy-lift transport helicopter
helicopter
variant of Mil Mi-10
airframeOrigin Mil Mi-6 NERFINISHED
countryOfOrigin Soviet Union
crew 3
cruiseSpeed 200 km/h
derivedFrom Mil Mi-6 NERFINISHED
designedBy Mikhail Mil NERFINISHED
developedIn 1960s
engineModel Soloviev D-25V NERFINISHED
engineType turboshaft
enteredService 1963
era Cold War
firstFlight 1960
hasVariant Mil Mi-10K NERFINISHED
height 7.8 m
landingGearType fixed tall four-leg landing gear
length 32.86 m
mainRotorConfiguration single main rotor with tail rotor
mainRotorDiameter 35 m
manufacturer Mil Moscow Helicopter Plant NERFINISHED
maximumSpeed 235 km/h
maximumTakeoffWeight 38000 kg
NATOReportingName Harke NERFINISHED
notableFeature ability to carry large external loads
ability to carry prefabricated structures
ability to carry vehicles as underslung loads
long spindly landing gear
shorter landing gear
numberOfEngines 2
payloadCapacity 15000 kg external load
primaryUser Soviet Air Force NERFINISHED
productionStatus out of production
range 250 km
role flying crane
flying crane
heavy-lift transport
serviceCeiling 3000 m
status retired from front-line service
tailConfiguration conventional tail with tail rotor
usedFor civil engineering projects
construction support
oil and gas industry support
transport of heavy equipment
transport of prefabricated buildings
transport of vehicles

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Mikhail Mil designed Mil Mi-10