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Spacecraft propellant dispenser for space debris disposal  id статьи: 3128
Тип публикации
материалы конференции
Язык
En
Журнал
AIP Conference Proceedings. 4th International Conference on Modernization, Innovations, Progress: Advanced Technologies in Material Science, Mechanical and Automation Engineering, MIP: Engineering 2022 Krasnoyarsk 12 April 2022 до 30 April 2022
Год
2024
Выходные данные
том 3021
выпуск 1
страницы № 020024
Авторы
Barkova, M.1
Zhukov, A.2
Kuznetsova, V.1
Gedzun, V.1
Bondareva, M.1
EDN
Абстракт
The article deals with the creation of a dispenser for supplying pseudo-liquid fuel from the engines of a spacecraft for collecting space debris. The dispenser differs from the existing ones in that it has a pulsed fuel supply method and consists of 4 nozzles coming from a drum-ball mill. Taking into account the effect of the induced difference in resistance of materials, which varies with time, is an urgent task of modern mechanics, since the destruction of structural elements occurs under the combined action of a load and a medium, which is a complex of physicochemical processes that occur on the surface and in the volume of the structural elements under study.
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Дата занесения
2024-05-23 10:34:05
Scopus
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2
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0.33
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