Spacecraft reflectors thermomechanical analysis

Spacecraft reflectors thermomechanical analysis

Xehetasun bibliografikoak
Parent link:	European Physical Journal Web of Conferences (EPJ Web of Conferences) Vol. 82 : Thermophysical Basis of Energy Technologies.— 2015.— [01005, 6 р.]
Erakunde egilea:	Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
Beste egile batzuk:	Ponomaryov V. S. Viktor Sergeevich, Gerasimov A. V. Aleksandr Vladimirovich, Ponomarev S. V. Sergey Vasiljevich, Shendalev D. O. Denis Olegovich
Gaia:	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.
Hizkuntza:	ingelesa
Argitaratua:	2015
Gaiak:	электронный ресурс труды учёных ТПУ
Sarrera elektronikoa:	http://dx.doi.org/10.1051/epjconf/20158201005
Formatua:	Baliabide elektronikoa Liburu kapitulua
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=642964

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