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The RD-107 and RD-108 engines are produced at the JSC Kuznetsov plant in Samara, Russia, under the supervision of the Privolzhskiy branch of NPO Energomash, also known as the Volga branch. [1] [3] [5] The Privolzhsky branch was organized as a branch of OKB-456 in 1958, specifically for the manufacture of RD-107 and RD-108 engines. The branch ...
The compressor spool, turbine and compressor, is in green. The free power turbine is in purple. A free-turbine turboshaft is a form of turboshaft or turboprop gas turbine engine where the power is extracted from the exhaust stream of a gas turbine by an independent turbine, downstream of the gas turbine. The power turbine is not mechanically ...
RD-93MA is a derivative of the RD-33 and is specifically designed for single engine light fighter jets. It uses the BARK-93MA automatic control system; Klimov VK-10M 22 to 24,200 lbf (97.87 - 107.647 kN) RD-35, agreement with Slovakian PSLM ZVL; RD-45; GTD-350; RD-500, copy of the Rolls-Royce Derwent V; TV2-117 (built by Isotov from 1959–1964 ...
The RD-191 is a single-chamber version used in the Russian Angara rocket. [11] Variants of RD-191 include RD-151 in South Korean Naro-1 rocket, [12] RD-181 in American Orbital ATK Antares rocket, and the proposed RD-193 for the Soyuz-2-1v project. [13]
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RD-0124 (GRAU Index 14D23). It is the version for the Soyuz 2.1b and Soyuz 2.1v Block I stage. It is the first liquid rocket engine designed in Russia after the Soviet period. [3] [citation needed] RD-0124A It is the version that powers the Angara URM-2, both the 1.2 and the bigger 5 versions. It differs on the base model in having an extended ...
Advanced variant that replaced the -300 model on non-export aircraft. [3] R-29BS-300. Variant with modified gearbox. Used in several export variants of the Sukhoi Su-17. [3] Khatchaturov R-35-300. Developed version used in late variants of the MiG-23. Shenyang WP-15. Chinese reverse-engineered copy of the R-29-300. [4]