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Designing corrections for the trajectory of the Spektr-R spacecraft in the event of immersions into the Moon’s sphere of influenceстатья
Информация о цитировании статьи получена из
Web of Science,
Scopus
Статья опубликована в журнале из списка Web of Science и/или Scopus
Дата последнего поиска статьи во внешних источниках: 7 декабря 2017 г.
- Авторы: Zaslavskii G.S., Zakhvatkin M.V., Kardashev N.S., Kovalev Yu Yu, Mikhailov E.A., Popov M.V., Sokolovskii K.V., Stepan’yants V.A., Tuchin A.G.
- Журнал: Cosmic Research (English translation of Kosimicheskie Issledovaniya)
- Том: 55
- Номер: 4
- Год издания: 2017
- Издательство: Pleiades Publishing, Inc.
- Местоположение издательства: New York, USA
- Первая страница: 290
- Последняя страница: 305
- DOI: 10.1134/s0010952517040050
- Аннотация: The results of updating the parameters of motion of the Spektr-R spacecraft at the end of 2016 have shown that, in January 2018, with a probability close to unity, the condition that a spacecraft stay in the Earth's shadow is violated; however, in May of the same year, the ballistic life of the spacecraft will be terminated. Thus, in 2017, the question arose of how to design the correction of flight of this spacecraft using its onboard propulsion system. The correction was designed with allowance for the fact that, for the first time since it was launched, the spacecraft in the course of several years, beginning with 2017, repeatedly approaches the Moon, deeply immersing into its sphere of influence. This paper presents the technologically and organizationally convenient, allowable versions of upcoming correction of the Spektr-R spacecraft trajectory and justifies the particular scheme of its implementation.
- Добавил в систему: Соколовский Кирилл Владимирович