Geodesic
Thermal-control system of experimental model of spacecraft optical telescope assembly
Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 9 (2013), pp. 236-243 Cet article a éte moissonné depuis la source Math-Net.Ru

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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.
Keywords: temperature, heat flow, thermal regime, strain
Mots-clés : objective. 
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S. V. Tsaplin; S. A. Bolychev. Thermal-control system of experimental model of spacecraft optical telescope assembly. Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 9 (2013), pp. 236-243. http://geodesic.mathdoc.fr/item/VSGU_2013_9_a27/

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