This article needs additional citations for
verification. (June 2021) |
D-136 | |
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The Ivchenko-Progress D-136 engine on display at the 2009 MAKS Air Show. | |
Type | Turboshaft |
National origin | Soviet Union |
Manufacturer | Ivchenko-Progress / Motor Sich |
Major applications | Mil Mi-26 |
Developed from | Lotarev D-36 |
Developed into | Progress D-236 |
The Lotarev D-136 is a turboshaft engine from the ZMKB Progress Design Bureau. The engine powers the Mil Mi-26 "Halo" helicopter. Development of the engine had begun in about 1972. [1]: 76 . The D-136 first flew on a production Mi-26 helicopter in 1980. [1]: 79
The core of the engine is identical to the Lotarev D-36 turbofan from which the D-136 is derived. [2]
Data from Mil's heavylift helicopters, [1] pages 90- 91
Related development
Comparable engines
Related lists
This article needs additional citations for
verification. (June 2021) |
D-136 | |
---|---|
![]() | |
The Ivchenko-Progress D-136 engine on display at the 2009 MAKS Air Show. | |
Type | Turboshaft |
National origin | Soviet Union |
Manufacturer | Ivchenko-Progress / Motor Sich |
Major applications | Mil Mi-26 |
Developed from | Lotarev D-36 |
Developed into | Progress D-236 |
The Lotarev D-136 is a turboshaft engine from the ZMKB Progress Design Bureau. The engine powers the Mil Mi-26 "Halo" helicopter. Development of the engine had begun in about 1972. [1]: 76 . The D-136 first flew on a production Mi-26 helicopter in 1980. [1]: 79
The core of the engine is identical to the Lotarev D-36 turbofan from which the D-136 is derived. [2]
Data from Mil's heavylift helicopters, [1] pages 90- 91
Related development
Comparable engines
Related lists