Spacecraft reflectors thermomechanical analysis; European Physical Journal Web of Conferences (EPJ Web of Conferences); Vol. 82 : Thermophysical Basis of Energy Technologies

Dettagli Bibliografici
Parent link:	European Physical Journal Web of Conferences (EPJ Web of Conferences) Vol. 82 : Thermophysical Basis of Energy Technologies.— 2015.— [01005, 6 р.]
Ente Autore:	Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
Altri autori:	Ponomaryov V. S. Viktor Sergeevich, Gerasimov A. V. Aleksandr Vladimirovich, Ponomarev S. V. Sergey Vasiljevich, Shendalev D. O. Denis Olegovich
Riassunto:	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.
Lingua:	inglese
Pubblicazione:	2015
Soggetti:	электронный ресурс труды учёных ТПУ
Accesso online:	http://dx.doi.org/10.1051/epjconf/20158201005
Natura:	Elettronico Capitolo di libro
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=642964

Descrizione
Riassunto:	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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