THERMAL-CONTROL SYSTEM OF EXPERIMENTAL MODEL OF SPACECRAFT OPTICAL TELESCOPE ASSEMBLY


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Abstract

Software on the base of program package of ANSYS, MathCAD, Zemax for study of influence of thermal factors of space factor on optical characteristics of lens objective of spacecraft is developed. Calculation of non-stationary field of temperature and deformation, output data of lens objective for specific case is carried out.

About the authors

S.V. Tsaplin

Samara State University

Author for correspondence.
Email: morenov.sv@ssau.ru

S.A. Bolychev

Samara State University

Email: morenov.sv@ssau.ru

References


Copyright (c) 2017 С.В. Цаплин, С.А. Болычев

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