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

About the authors

A D Novikov

Bauman Moscow State Technical University (National Research University)

Author for correspondence.
Email: novikov.andrey.sm13@gmail.com

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

2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

P V Prosuntsov

Bauman Moscow State Technical University (National Research University)

Email: pavel.prosuntsov@mail.ru

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.

2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

S V Reznik

Bauman Moscow State Technical University (National Research University)

Email: sreznik@bmstu.ru

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.

2-nd Baumanskaya str., 5/1, Moscow, Russia, 105005

References

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Copyright (c) 2017 Novikov A.D., Prosuntsov P.V., Reznik S.V.

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