Scientific technological module of plasma injection for microsatellite
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1Sorokin, AF, 1Tsyukh, AM, 1Nesteruk, VN, 2Vlasenko, VP, 1Zaluzhnyj, RN, 3Sorokin, AA, 4Zakharova, MY, 5Arsentiev, IN, 5Tarasov, IS 1National Center of Space Facilities Control and Test of the State Space Agency of Ukraine, Yevpatoria, AR Crimea, Ukraine 2National Center of Space Facilities Control and Test, Kyiv, Ukraine 3V.I. Vernadsky Taurian National University, Simferopol, Ukraine 4Scientific Production Enterprise ST «TIAMAS» (Russia-Ukraine), Yevpatoria, Crimea, Ukraine 5Ioffe Institute of the Russian Academy of Sciences, St. Petersburg, Russia |
Kosm. nauka tehnol. 2006, 12 ;(2-3):008-011 |
https://doi.org/10.15407/knit2006.02.008 |
Publication Language: Russian |
Abstract: The possibility to accommodate aboard a microsatellite a multifunctional module consisting of a plasma injector and heterolaser is considered. It is shown that a module of this kind allows one not only to make orbit correction and microsatellite orientation but also may be used in active space experiments.
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Keywords: heterolaser, microsatellite, plasma injector |
References:
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