Email this article Implementation featuresof deploy able multibeam aerospace antenna
- Authors: Bey NA1, Zimin VN1, Krylov AV1, Meshkovsky VE1, Churilin SA1
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- Issue: Vol 11, No 3 (2010)
- Pages: 102-104
- Section: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508588
- ID: 508588
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Abstract
A variant of Russian multibeam aerospace antenna for satellite communication system of geostationary spacecraft is under consideration in this article. The results of mirror surface numerical optimization and analysis for main strength parameters of multibeam antenna module under launching dynamic forces are presented here
About the authors
N A Bey
Email: bei@mx.bmstu.ru <mailto:bei@mx.bmstu.ru>
V N Zimin
Email: niism@sm.bmstu.ru <mailto:niism@sm.bmstu.ru>
A V Krylov
Email: sml @sm.bmstu.ru <mailto:sm1@sm.bmstu.ru>
V E Meshkovsky
Email: sml l@sm.bmstu.ru <mailto:sm11@sm.bmstu.ru>
S A Churilin
References
- Аносов А. М.,БейН. А.,ВечтомовВ. А. Применение бортовых многолучевых антенн в системах спутниковой связи//Антенны. 2005. № 10. С. 19-23.
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