Analysis of the cyclogram of maintaining a low working orbit of a space-craft of the AIST-2 class using an electric jet engine
A study was made of the time parameters of the cyclogram for maintaining the low working orbit of a small spacecraft of the AIST-2 class using an electric jet engine. The analysis is made for working orbits with a height in the range from four hundred to five hundred kilometers with a changing upper...
| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
Association «Technology Platform «National Information Satellite System»
2020-09-01
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| Series: | Космические аппараты и технологии |
| Subjects: | |
| Online Access: | http://journal-niss.ru/en/archive_view.php?num=221 |