An attempt to develop and build composite structural elements for an electro-optical module of a spacecraft
Автор: Akkuratov Igor Leonidovich, Alyamovsky Andrey Ivanovich, Davydov Dmitry Yaroslavovich, Zaprudnov Dmitry Modestovich, Kopyl Nikolay Ivanovich, Senkovsky Alexander Nikolayevich, Chernyavsky Alexander Grigoryevich
Журнал: Космическая техника и технологии @ktt-energia
Рубрика: Материалы, производство и технологии изделий РКТ
Статья в выпуске: 1 (4), 2014 года.
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The paper presents results of engineering and manufacturing process studies for various design variants of structural elements for an electro-optical module. The structural element design that was selected consisted in honeycomb sandwich structure with base layers made of high-modulus carbon fiber reinforced plastic. The manufacturing process was developed and tested. The selected design and manufacturing solutions have been confirmed by the results of ground stand-alone tests.
Structural elements, carbon plastic, supporting layers, coefficient of linear thermal expansion, characteristics of specific strength and hardness, honeycomb sandwich structure
Короткий адрес: https://sciup.org/14343436
IDR: 14343436
