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ELECTROJET THRUSTER TO BALANCE AN AERODYNAMIC DRAG ON A SMALL SPACECRAFT IN A VERY LOW EARTH ORBIT

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 obstacle to their use is a gas-dynamic drag on a spa...

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Bibliographic Details
Date:	2026
Main Author:	GRYSHKEVYCH, O. D.
Format:	Article
Published:	текст 3 2026
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

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