Soloviev D-25

D-25
Type Turboshaft
Manufacturer Soloviev Design Bureau
First run 1954
Major applications Mil Mi-6.



The Soloviev D-25V is a Soviet gas-turbine turboshaft engine for use in large helicopters. Designed and originally manufactured by the Soloviev Design Bureau the engine has been in production since May 1960.

The V in the designation means vertoletny (Russian: Вертолетный), for helicopters.

Variants

D-25V
Standard helicopter use production engines
D-25VF
Additional compressor zero-stage, power output 6,500 hp (4,847 kW)
D-25VK
A combined propeller and shaft output engine for the Kamov Ka-22 developing 5,500 hp (4,101 kW)

Applications

Specifications (D-25V)

Data from Gunston.[1]

General characteristics

Components

Performance

See also


Comparable engines
Related lists

References

Notes

  1. Gunston 1989, p. 164.

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

External links

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