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