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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 ...
RD-107, RD-108—Soviet engine type developed in the 1950s, used on R-7 family vehicles including the active Soyuz-2. [1] F-1—RP-1/LOX engine used on the first stage of Saturn V. Most powerful single combustion chamber liquid-fueled engine ever flown. [2] J-2—Upper stage LH2/LOX engine developed in the 1960s and used on Saturn V.
English: A turbine and gear box are mounted in a casing called a nacelle, and rotor blades are attached to the turbine. The turbine localizes the energy of the turning rotor blades in a single rotating shaft that generates electricity.
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 ...
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1 set of turbines and pumps; turbine produces approximately 257,000 hp (192 MW); equivalent to the power output of 3 nuclear-powered icebreakers; Ignition: pyrophoric start-up fuel capsule (triethylaluminium) [17] Vacuum thrust: 7,887 kN (1,773,000 lb f) Vacuum I sp: 338 s (3.31 km/s) Sea-level I sp: 309 s (3.03 km/s)