TitleFeatures of the temperature control system of the small spacecraft «Yubileyniy-2»
AuthorsS.A. Ganenko, V.V. Basynin, Z.A. Kazantsev
OrganizationSiberian State Aerospace University
AbstractWe have developed a methodology for the conduction of thermobalanced and electrothermovacuum tests of the satellite of non-hermetic performance. We have received a high accuracy of the convergence of the results of mathematical calculations and experimental data for an accurate imitation of space.
Keywordssystems of thermal regulation, heat pipe
For citing this articleGanenko S.A., Basynin V.V., Kazantsev Z.A. Features of the temperature control system of the small spacecraft «Yubileyniy-2» // The Research of the Science City, 2012, no. 2, pp. 17-19.
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