Spacecraft reflectors thermomechanical analysis

Bibliographic Details
Parent link:	European Physical Journal Web of Conferences (EPJ Web of Conferences) Vol. 82 : Thermophysical Basis of Energy Technologies.— 2015.— [01005, 6 р.]
Corporate Author:	Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
Other Authors:	Ponomaryov V. S. Viktor Sergeevich, Gerasimov A. V. Aleksandr Vladimirovich, Ponomarev S. V. Sergey Vasiljevich, Shendalev D. O. Denis Olegovich
Summary:	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.
Published:	2015
Subjects:	электронный ресурс труды учёных ТПУ
Online Access:	http://dx.doi.org/10.1051/epjconf/20158201005
Format:	Electronic Book Chapter
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=642964

Description
Summary:	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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