СИСТЕМА ОБЕСПЕЧЕНИЯ ТЕПЛОВОГО РЕЖИМА ЭКСПЕРИМЕНТАЛЬНОЙ МОДЕЛИ ОПТИКО-ТЕЛЕСКОПИЧЕСКОГО КОМПЛЕКСА КОСМИЧЕСКОГО АППАРАТА

S.V. Tsaplin; Цаплин С.В.; S.A. Bolychev; Болычев С.А.

doi:10.18287/2541-7525-2013-19-9.2-236-243

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

Authors: Tsaplin S.¹, Bolychev S.¹
Affiliations:
1. Samara State University
Issue: Vol 19, No 9.2 (2013)
Pages: 236-243
Section: Articles
URL: https://journals.ssau.ru/est/article/view/4731
DOI: https://doi.org/10.18287/2541-7525-2013-19-9.2-236-243
ID: 4731

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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.