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The Mikoyan MiG-35 (Russian: Микоян МиГ-35; NATO reporting name: Fulcrum-F) is a Russian multirole fighter that is designed by Mikoyan, a division of the United Aircraft Corporation (UAC). Marketed as a 4++ generation jet fighter , it is a further development of the MiG-29M/M2 and MiG-29K/KUB fighters.
The Klimov RD-33 is a turbofan jet engine for a lightweight fighter jet and which is the primary engine for the Mikoyan MiG-29 and CAC/PAC JF-17 Thunder.It was developed in OKB-117 led by S. P. Izotov (now OAO Klimov) from 1968 with production starting in 1981.
MiG I-340/SM-1 - prototype version of MiG-17 with two Mikulin AM-5 engines, 1952; led to the MiG-19 MiG I-350 (M) - fighter prototype, 1951; first Soviet fighter to maintain supersonic speed MiG I-360/SM-2 - derivative of I-350, powered by Mikulin AM-5 engines, 1952
The Mikulin AM-35 was a 1930s Soviet piston aircraft engine. [1] Derived from the AM-34FRN , the AM-35 entered production in 1940 and was used on the MiG-1 and MiG-3 World War II fighters as well as the Petlyakov Pe-8 heavy bomber .
Like the MiG-25, the MiG-31 is a large twin-engine aircraft with side-mounted air intake ramps, a shoulder-mounted wing with an aspect ratio of 2.94, and twin vertical tailfins. Unlike the MiG-25, it has two seats, with the rear occupied by a dedicated weapon systems officer. [26] The MiG-31 was designed to fulfill the following mission ...
The aircraft was developed from Mikoyan's E-721. Developed by the United Aircraft Corporation (OAK), this light fighter was believed to incorporate an 11-ton thrust VK-10M engine based on the RD-33MK-35 engine used by the MiG-35. This new updated engine would be manufactured at the Klimov factory. The engine is supposed to be fifth generation ...
The U.S. Air Force isn't building a new F-35 engine after all. Skip to main content. Sign in. Mail. 24/7 Help. For premium support please call: 800-290-4726 more ways to ...
Tumansky R-35 The Tumansky R-29 is a Soviet turbojet aircraft engine that was developed in the early 1970s. [ 1 ] It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.