SPACECRAFT DISPOSAL IN QUASI-GEOSTATIONARY ORBIT
The results of simulation of the process of the disposal (post-mission disposal or disposal after failure as a result of emergency) of a spacecraft in quasi-geostationary orbit are given. The necessary impulses, fuel consumption for maneuvers, the required time for the raising the orbit to 300 km,...
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| Главный автор: | |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
Buketov Karaganda National Research University
2018-03-01
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| Серии: | Eurasian Physical Technical Journal |
| Предметы: | |
| Online-ссылка: | https://phtj.buketov.edu.kz/EPTJ/article/view/498 |
| Метки: |
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