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Klimov VK-1
Klimov RD-45
Shenyang PF-1


Klimov VK-1


Immediately after World War II, the Soviet Union manufactured copies of first generation German Junkers 004 and BMW 003 engines, which were advanced designs with poor durability, limited by Germany's availability of rare metals at wartime. However in 1946, before the Cold War had really begun, the new British Labour government under the Prime Minister, Clement Attlee, keen to improve diplomatic relations with the Soviet Union, authorised Rolls-Royce to export 40 Rolls-Royce Nene centrifugal flow turbojet engines. In 1958 it was discovered during a visit to Beijing by Whitney Straight, then deputy chairman of Rolls-Royce, that this engine had been copied without license to power the MiG-15 'Fagot', first as the RD-45, and after initial problems of metallurgy forced the Soviet engineers to develop a slightly redesigned (and metallurgically closer) copy, the engine had then entered production as the Klimov VK-1 (Rolls-Royce later attempted to claim £207m in license fees, without success).

It was developed by Vladimir Yakovlevich Klimov and first produced by the GAZ 116 works.

The RD-45 was further improved to produce the VK-1, which differed from the Nene in having larger combustion chambers, larger turbine, and revised airflow through the engine. The VK-1F added the afterburner.

The engine featured a centrifugal compressor, requiring a larger-diameter fuselage than aircraft featuring the more progressive axial compressor designs that had already appeared in WWII Germany and Britain. The engine was built under license in China as the WP-5.


The VK-1 was used to power MiG-15 'Fagot' and MiG-17 'Fresco' fighters, as well as the Il-28 'Beagle'.


Type: Turbojet
Length: 2,600 mm (102 in)
Diameter: 1,300 mm (51 in)
Dry weight: 872 kg (1,395 lb)
Compressor: Centrifugal compressor
Maximum thrust: 26.5 kN (5,955 lbf)
Specific fuel consumption: 109.1 kg/(kN·h) (1.07 lb/(lbf·h))
Thrust-to-weight ratio: 41.4 N/kg (4.27:1)



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