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The M-105 was the first Klimov V-12 engine design to use reverse-flow cylinder heads, forcing the induction system to be placed on the outside of the cylinder banks, with the exhaust system also exiting from the outboard side, with twin sets of "siamesed" exhaust ports adjacent to each other. About 129,000 M-105 and its variants were built.
Pages in category "Soviet and Russian aircraft engines" The following 8 pages are in this category, out of 8 total. This list may not reflect recent changes. C.
Klimov United Engine Company is now located in Saint Petersburg. It used the nationalised buildings originally erected by 1914 in the city's present-day Vyborgsky District for the joint stock Russian Renault automotive works, [ 4 ] [ 5 ] adding new workshop and administrative premises on the land in Bolshoy Sampsoniyevskiy Prospect avenue near ...
Soviet and Russian aircraft engines (10 C, 8 P) U. United Engine Corporation (3 C, 9 P) Pages in category "Aircraft engine manufacturers of Russia"
Kuznetsov's most powerful aviation engine is the Kuznetsov NK-321 that propels the Tupolev Tu-160 bomber and was formerly used in the later models of the Tu-144 supersonic transport (an SST that is now obsolete and no longer flown). The NK-321 produced a maximum of about 245 kN (55,000 lb f) of thrust. Kuznetsov aircraft engines include:
The M-17 was the most powerful engine available to the Soviet aircraft industry and it was in high demand, so much that Factory No. 24 in Moscow also began to build the M-17. 165 engines were produced in 1930 at Rybinsk and Factory No. 24 had managed to build its first three engines by June 1930.
The Vedeneyev M14P is a Russian nine-cylinder, four-stroke, air-cooled, petrol-powered radial engine. Producing 360 hp (268 kW), its design dates from the 1940s (Kotelnikov 2005), and is itself a development of the Ivchenko AI-14 engine. The engine has been used extensively by the Yakovlev and Sukhoi Design Bureaus.
These powerful engines also allowed the large and complex interceptor to attain supersonic speeds at low altitudes under 1,500 m (4,900 ft). Data from: Aircraft engines of the World 1970, [6] Jane's all the World's Aircraft 1993–94 [7] Other Variants D-30V12 High-altitude version for the Myasishchev M-55 de-rated to 49 kN (11,000 lbf) [8] D-30F11