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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| Datum: | 2026 |
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| Format: | Artikel |
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текст 3
2026
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| Online Zugang: | https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/190 |
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| Назва журналу: | Technical Mechanics |