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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.
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.
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.
TV7-117S 2800 hp; TV7-117SM/ST (the S stands for the Russian word for aircraft, the M for airliner, as opposed to military cargo aircraft, which are designated ST, with the T being for transport) is the turboprop variant for fixed wing aircraft, that was introduced by Klimov in 2002, featuring a Full Authority Digital Electric Control system based on the BARK-12 or BARK-57 electronic engine ...
The engine entered production in 1940 and saw service in a number of Soviet aircraft. It powered the Tupolev Tu-2 and Pe-8 bombers and the inline engine -powered LaGG-3 was adapted for the ASh-82 producing the famous Lavochkin La-5 fighter and its development, Lavochkin La-7 , additionally the Lavochkin La-9 with its Lavochkin La-11 escort ...
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"
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.
VK-2500-01 Has a 1,500 shp (1,119 kW) maximum continuous performance and a 2,000 shp (1,491 kW) take-off performance. Powers Ka-52. [2]VK-2500-02