Samara University Repository
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This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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| Title: | Испытания разъемных соединений для труб малого диаметра двигательных установок космических аппаратов |
| Authors: | Васильева В. А. Назарова Я. А. |
| Keywords: | двигательные установки герметичность трубопроводы разъемные резьбовые соединения пневмогидравлические соединения параметры испытаний космические аппараты test parameters space technology propulsion systems pneumatic-hydraulic connections pipelines detachable threaded connections tightness |
| Issue Date: | 2025 |
| Citation: | Васильева, В. А. Испытания разъемных соединений для труб малого диаметра двигательных установок космических аппаратов = Testing of detachable joints for small diameter pipes of spacecraft thrusters / В. А. Васильева, Я. А. Назарова // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 55-57. |
| Abstract: | In order to increase the manufacturability of the propulsion systems of small spacecraft and reduce the cost of their manufacture, a detachable threaded connection was made, which is used to connect the pneumohydraulic elements included in these thrusters. The connection has successfully passed pneumatic, climatic and mechanical tests without destruction and significant changes in the diameter of the passage section of the tubes. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43245 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-55-57.pdf | 285.74 kB | Adobe PDF | View/Open |
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