MIRROR SPACE ANTENNA REFLECTOR MADE OF COMPOSITE MATERIALS CONSTRUCTIVE APPEARANCE DETERMINATION

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Abstract


This article describes search studies of optimal design and technological solutions for the ultralight mirror space antenna reflectors made of CFRP. The studies included finite element modeling of the reflector temperature and stress-strain state in the geostationary orbit. As a result of comparing the results of a number reflector variants modeling, a design was chosen, with minimal values of temperature displacements and linear density


A D Novikov

Principal contact for editorial correspondence.
novikov.andrey.sm13@gmail.com
Bauman Moscow State Technical University (National Research University) 2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

Novikov Andrey Dmitrievich, post graduate student, assistant professor of the department SM13 “Rocket and space composite structures” of the Bauman Moscow State Technical Un iversity. Research interests: design, producing and testing of space composite structures

P V Prosuntsov

pavel.prosuntsov@mail.ru
Bauman Moscow State Technical University (National Research University) 2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

Prosuntsov Pavel Viktorovich, Doctor of Technical Sciences, professor of the department SM13 “Rocket and space composite structures” of the Bauman Moscow State Technical University. Research interests: modeling and identification of thermal processes in rocket and spacecraft structures.

S V Reznik

sreznik@bmstu.ru
Bauman Moscow State Technical University (National Research University) 2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

Reznik Sergey Vasilyevich, Doctor of Technical Sciences, pr ofessor, head of the department SM13 “Rocket and space composite str uctures” of the Bauman Moscow St ate Technical University. Research interests: design, producing and testing of rocket and space composite structures.

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