Spacecraft reflectors thermomechanical analysis

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Spacecraft reflectors thermomechanical analysis	753 KB	Adobe Acrobat PDF	Read	Download
DOI Доступ к ресурсу на сайте издателя			10.1051/epjconf/20158201005

Title: Spacecraft reflectors thermomechanical analysis
Creator: Ponomarev, Viktor S.
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Ponomarev, Sergey V. (доктор физ.-мат. наук)
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Shendalev, Denis O.
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Gerasimov, Alexander V.
Date: 2015
DOI: 10.1051/epjconf/20158201005
Description: In this article, thermo-mechanical analysis results of the composite reflectors for the use on the geostationary Earth orbit possibility studies are described. The behavior of two different space reflector structures manufactured on composite materials is investigated. The estimates of reflecting surfaces RMS deviations for the two extreme cases orbital inclinations are presented.

Created: 11-10-2016

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