DEPLOYMENT OF THE ROTATING TWO BODIES TETHER IN AN ORBIT
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 connecting cable is assumed massless. The ai...
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| Date: | 2026 |
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| Main Authors: | , |
| Format: | Article |
| Published: |
текст 3
2026
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| 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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