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  1. RD-0146 - Wikipedia

    'Rocket Engine 0146') is a liquid-fuel cryogenic rocket engine developed by KBKhA Kosberg in Voronezh, Russia. The RD-0146 is the first Russian rocket engine to burn liquid oxygen and …

  2. RD-0146 rocket engine - RussianSpaceWeb.com

    The RD-0146 became the first Russian rocket engine without a gas generator, and it was also equipped with extendable nozzle extension without a coooling system and it was capable of …

  3. RD-0146 - Encyclopedia Astronautica

    The RD-0146 thrust level fell between those of Pratt & Whitney's workhorse RL-10 and the cancelled Euro-American SPW-2000. As of 2007 the engine was being marketed for use in …

  4. While work on the RO-95 engine was stopped after preliminary design, this engine might be considered as a predecessor to the first modern Russian expander cycle LOX-LH2 RD0146 …

  5. Single-shaft and double-shaft TPA configurations implemented in the RD-120, SSME and RD-0146 engines are described. The criteria used in selecting single-shaft and double-shaft TPA …

  6. Development Trend of Liquid Hydrogen-Fueled Rocket Engines …

    RD-0146. The RD-0146 engine is the hydrogen-fueled engine of Russia in the expander cycle, in which turbopumps are driven by waste heat absorbed in the nozzle and combustion chamber, …

  7. RD-0146 and a history of Russian hydrogen rocketry

    Dec 30, 2021 · A substantial update and history on Russian hydrogen rocketry; the RD-0146 started out almost literally as a Russian RL-10 but it appears technology transfer issues …

  8. RD-0146: The First LOX-LH2 Expander Cycle Liquid Rocket Engine

    considered as a predecessor to the first modern Russian expander cycle LOX-LH2 RD0146 engine. After 10 years, the Russian rocket companies returned to the expander cycle of LOX …

  9. RD-0146 - 卫星百科,很认真的中文航天百科 - 灰机wiki - 北京嘉 …

    RD-0146 是俄罗斯研发的一种氢氧发动机,是苏联/俄罗斯的第一个膨胀循环氢氧发动机。 1988年,应 能源火箭公司 的要求,化工自动设计局开始一个膨胀循环氢氧发动机的研制工作。 该发 …

  10. About: RD-0146 - DBpedia Association

    The RD-0146 is the first Russian rocket engine to burn liquid oxygen and liquid hydrogen in the expander cycle, in which turbopumps are driven by waste heat absorbed in the nozzle and …

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