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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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Bibliographic Details
Date:	2026
Main Authors:	WANG, Ch., ZAKRZHEVSKYI, O. E.
Format:	Article
Published:	текст 3 2026
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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