Methodology of designing a small spacecraft for technological purposes
The paper presents a methodology for designing a small spacecraft to perform the tasks of technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that it will be equipped with a microgravity platform to meet the requirements for micro-accelerations. The...
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| Format: | Article |
| Language: | English |
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Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2024-12-01
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| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2024/%D0%A2.8,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/73-79%20%D0%A1%D0%B5%D0%B4%D0%B5%D0%BB%D1%8C%D0%BD%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%90.%20%D0%92.,%20%D0%A2%D0%B0%D0%BD%D0%B5%D0%B5%D0%B2%D0%B0%20%D0%90.%20%D0%A1..pdf |
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| _version_ | 1832543954462048256 |
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| author | A. V. Sedelnikov A. S. Taneeva |
| author_facet | A. V. Sedelnikov A. S. Taneeva |
| author_sort | A. V. Sedelnikov |
| collection | DOAJ |
| description | The paper presents a methodology for designing a small spacecraft to perform the tasks of
technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that
it will be equipped with a microgravity platform to meet the requirements for micro-accelerations.
The methodology is based on the principles of individuality, attainability and controllability. They
guarantee the maximum possible consideration of the features of the gravity-sensitive process
being implemented, including compliance with the requirements for limiting the micro-acceleration
module in the working area of technological equipment and effective control of this implementation.
The developed technique can be used in the design of a small spacecraft for technological purposes. |
| format | Article |
| id | doaj-art-df4f717f942d41caae2a33afe67060cf |
| institution | Kabale University |
| issn | 2588-0373 2587-764X |
| language | English |
| publishDate | 2024-12-01 |
| publisher | Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education |
| record_format | Article |
| series | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| spelling | doaj-art-df4f717f942d41caae2a33afe67060cf2025-02-03T11:20:36ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2024-12-0184737910.25206/2588-0373-2024-8-4-73-79Methodology of designing a small spacecraft for technological purposesA. V. Sedelnikov0https://orcid.org/0000-0003-2698-1348A. S. Taneeva1https://orcid.org/0000-0002-8531-760XSamara National Research UniversitySamara National Research UniversityThe paper presents a methodology for designing a small spacecraft to perform the tasks of technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that it will be equipped with a microgravity platform to meet the requirements for micro-accelerations. The methodology is based on the principles of individuality, attainability and controllability. They guarantee the maximum possible consideration of the features of the gravity-sensitive process being implemented, including compliance with the requirements for limiting the micro-acceleration module in the working area of technological equipment and effective control of this implementation. The developed technique can be used in the design of a small spacecraft for technological purposes.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2024/%D0%A2.8,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/73-79%20%D0%A1%D0%B5%D0%B4%D0%B5%D0%BB%D1%8C%D0%BD%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%90.%20%D0%92.,%20%D0%A2%D0%B0%D0%BD%D0%B5%D0%B5%D0%B2%D0%B0%20%D0%90.%20%D0%A1..pdfdesign methodologymicro-accelerationgravity-sensitive processesmicrogravity platformsmall spacecrafttechnological purposevibration protection device |
| spellingShingle | A. V. Sedelnikov A. S. Taneeva Methodology of designing a small spacecraft for technological purposes Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" design methodology micro-acceleration gravity-sensitive processes microgravity platform small spacecraft technological purpose vibration protection device |
| title | Methodology of designing a small spacecraft for technological purposes |
| title_full | Methodology of designing a small spacecraft for technological purposes |
| title_fullStr | Methodology of designing a small spacecraft for technological purposes |
| title_full_unstemmed | Methodology of designing a small spacecraft for technological purposes |
| title_short | Methodology of designing a small spacecraft for technological purposes |
| title_sort | methodology of designing a small spacecraft for technological purposes |
| topic | design methodology micro-acceleration gravity-sensitive processes microgravity platform small spacecraft technological purpose vibration protection device |
| url | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2024/%D0%A2.8,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/73-79%20%D0%A1%D0%B5%D0%B4%D0%B5%D0%BB%D1%8C%D0%BD%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%90.%20%D0%92.,%20%D0%A2%D0%B0%D0%BD%D0%B5%D0%B5%D0%B2%D0%B0%20%D0%90.%20%D0%A1..pdf |
| work_keys_str_mv | AT avsedelnikov methodologyofdesigningasmallspacecraftfortechnologicalpurposes AT astaneeva methodologyofdesigningasmallspacecraftfortechnologicalpurposes |