ЕЛЕКТРОРЕАКТИВНИЙ ДВИГУН ДЛЯ КОМПЕНСАЦІЇ АЕРОДИНАМІЧНОГО ГАЛЬМУВАННЯ МАЛОГО КОСМІЧНОГО АПАРАТА НА НАДНИЗЬКІЙ ОРБІТІ

DOI: https://doi.org/10.15407/itm2026.02.049 The goal of this paper is to study the feasibility of an electrojet thruster for a long-term operation in a very low Earth orbit. The paper presents the advantages of very low orbits and substantiates the importance of their exploitation. The main obstacl...

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Bibliographic Details
Date:2026
Main Author: GRYSHKEVYCH, O. D.
Format: Article
Language:Ukrainian
Published: текст 3 2026
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Online Access:https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/190
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Journal Title:Technical Mechanics
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Technical Mechanics