Thermal deformations of a glass spherical satellite


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Abstract

The effect of the kind of the reflecting coating of a glass spherical satellite on thermal deformations caused by the solar irradiation is considered. Two types of coating deposited on one of the hemispheres are considered: aluminum with a protective layer of bakelite varnish and interference dielectric coating for two orientations of the satellite orbit. Structures of a multilayer dielectric coating and technologies of its deposition are described.

About the authors

V. P. Vasiliev

JSC Research and Production Corporation “Precision Systems and Instruments,”

Email: alsokolov@bk.ru
Russian Federation, Moscow, 111024

V. D. Nenadovich

JSC Research and Production Corporation “Precision Systems and Instruments,”

Email: alsokolov@bk.ru
Russian Federation, Moscow, 111024

V. V. Murashkin

JSC Research and Production Corporation “Precision Systems and Instruments,”

Email: alsokolov@bk.ru
Russian Federation, Moscow, 111024

A. L. Sokolov

JSC Research and Production Corporation “Precision Systems and Instruments,”

Author for correspondence.
Email: alsokolov@bk.ru
Russian Federation, Moscow, 111024

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