Article

Cover

Title

Features of the temperature control system of the small spacecraft «Yubileyniy-2»

Authors

S.A. Ganenko, V.V. Basynin, Z.A. Kazantsev

Organization

Siberian State Aerospace University
Krasnoyarsk, Russia

Abstract

We 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.

Keywords

systems of thermal regulation, heat pipe

For citing this article

Ganenko 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.

This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).