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РОЗГОРТАННЯ ЗВ’ЯЗКИ ДВОХ ТІЛ, ЩО ОБЕРТАЄТЬСЯ, НА ОРБІТІ

DOI: https://doi.org/10.15407/itm2026.02.023 The focus of the study is a compact orbital tether consisting of two bodies that must be deployed from a spacecraft so that after deployment it rotates at a constant angular speed and attains a prescribed length. The end masses are taken as equal, and the...

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Bibliographic Details
Date:2026
Author Affiliations:
  • Ch. WANG — https://orcid.org/0000-0002-1358-7731 Northwestern Polytechnical University 1.127 YouyiXilu, Xi'an 710072 Shaanxi, P. R. China; e-mail: wangcq@nwpu.edu.cn
  • O. E. ZAKRZHEVSKYI — https://orcid.org/0000-0003-2106-2086 Space Research Institute of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine Kiev 03680, Ukraine; e-mail: alex.e.zakr@gmail.com
Keywords:keywords
Main Authors: WANG, Ch., ZAKRZHEVSKYI, O. E.
Format: Article
Language:English
Published: текст 3 2026
Subjects:
космічний трос
розгортання
обертання
динаміка
управління.
Online Access:https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/188
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Journal Title:Technical Mechanics
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Technical Mechanics

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https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/188

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