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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| Date: | 2026 |
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| Main Authors: | , |
| Format: | Article |
| Language: | English |
| Published: |
текст 3
2026
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| Subjects: | |
| Online Access: | https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/188 |
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| Journal Title: | Technical Mechanics |
| Download file: |  |