File:RD-119.jpg
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Русский: Жидкостный ракетный двигатель РД-119 в экспозиции музея истории космонавтики имени К. Э. Циолковского.
Жидкостный ракетный двигатель РД-119 разработан в 1958 – 1962 гг. в ОКБ-456 (ныне Научно-производственное объединение «Энергомаш») под руководством Главного конструктора Валентина Петровича Глушко. В состав РД-119 входят: камера, турбонасосный агрегат, газогенератор, рулевые сопла, агрегаты управления. Двигатель массой 179 кг и тягой 105 килоньютонов использует жидкий кислород и несимметричный диметилгидразин. Он применялся на второй ступени ракеты-носителя лёгкого класса «Космос». С его помощью небольшие спутники массой до 600 кг выводились на околоземные орбиты высотой примерно 200 км.English: Liquid rocket engine RD-119 in the exposition of the Museum of the History of Cosmonautics named after K. E. Tsiolkovsky. The RD-119 liquid rocket engine was developed in 1958-1962 at OKB–456 (now Energomash Research and Production Association) under the leadership of Chief Designer Valentin Petrovich Glushko. The RD-119 consists of: a chamber, a turbopump unit, a gas generator, steering nozzles, control units. The engine with a mass of 179 kg and a thrust of 105 kilonewtons uses liquid oxygen and asymmetric dimethylhydrazine. It was used on the second stage of the Kosmos light class launch vehicle. With its help, small satellites weighing up to 600 kg were launched into near-Earth orbits with a height of about 200 km. |
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| Source | Own work |
| Author | Stolbovsky |
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This image was uploaded as part of Russian Science Photo Competition 2022.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
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| current | 18:32, 8 May 2022 | | 3,394 × 5,091 (9.31 MB) | Stolbovsky (talk | contribs) | Uploaded own work with UploadWizard |
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