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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Bibliographic Details
Main Authors: A. V. Sedelnikov, A. S. Taneeva
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2024-12-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
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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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