Spacecraft reflectors thermomechanical analysis

Spacecraft reflectors thermomechanical analysis

書誌詳細
Parent link:European Physical Journal Web of Conferences (EPJ Web of Conferences)
Vol. 82 : Thermophysical Basis of Energy Technologies.— 2015.— [01005, 6 р.]
団体著者: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
その他の著者: Ponomaryov V. S. Viktor Sergeevich, Gerasimov A. V. Aleksandr Vladimirovich, Ponomarev S. V. Sergey Vasiljevich, Shendalev D. O. Denis Olegovich
要約:Title screen
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.
言語:英語
出版事項: 2015
主題:
электронный ресурс
труды учёных ТПУ
オンライン･アクセス:http://dx.doi.org/10.1051/epjconf/20158201005
フォーマット: 電子媒体 図書の章
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=642964
その他の書誌記述
要約:Title screen
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.
DOI:10.1051/epjconf/20158201005

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