Lotarev D-136

E1030528

The Lotarev D-136 is a powerful turboshaft engine developed in the Soviet Union, best known for powering the heavy-lift Mil Mi-26 helicopter.

All labels observed (1)

Label Occurrences
Lotarev D-136 canonical 2

How this entity was disambiguated

Statements (44)

Predicate Object
instanceOf turboshaft engine
alsoKnownAs Progress D-136
applicationType rotorcraft
associatedWith Mil Moscow Helicopter Plant
category Soviet aircraft engines
helicopter engines
turboshaft engines
compressorType axial-flow compressor
configuration axial-flow turboshaft
coolingMethod air-cooled
coolingSystem air-cooled turbine
countryOfOrigin Soviet Union
designBureau Ivchenko-Progress
designGoal provide very high power for heavy-lift helicopters
developer Lotarev Design Bureau
era Cold War
family Lotarev D-136 engine family
fuelType jet fuel
intendedRole heavy-lift helicopter powerplant
manufacturer Motor Sich
marketedBy Ivchenko-Progress
mounting twin-engine installation on Mil Mi-26
notableFeature designed for very heavy-lift operations
high power-to-weight ratio
notableFor powering the world’s heaviest-lift production helicopter
numberOfCompressorStages 12
powerClass high-power turboshaft
powerTransmission to main rotor via gearbox
primaryApplication Mil Mi-26
regionOfUse Russia
export markets
former Soviet republics
serviceEntry late 1970s
shaftPower 8200 kW
approximately 11000 shp
status in service
successor D-136-2
turbineType free power turbine
usedBy Russian Air Force
Soviet Air Force
linked to: Soviet Air Forces

various civilian operators
usedOnAircraft Mil Mi-26
Mil Mi-26T
linked to: Mil Mi-26

Mil Mi-26T2
linked to: Mi-26T2

How these facts were elicited

Referenced by (2)

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

Mil Mi-26 engineModel Lotarev D-136
Mil Mi-26 engineModel Lotarev D-136
subject linked to: Halo