Experimental simulation of nanosatellites heat modes
Keywords:
spacecraft, nano-satellite, thermal vacuum tests
Abstract
The technology of thermal modes modelling for nanosatellite (NS) PolyITAN-1 has been developed and thermal vacuum tests have been carried out. The results have shown that the simulation of the NS orbit and space factors is correct and confirmed that NS nodes and elements are operable under the specified conditions.
Published
2013-06-14
How to Cite
Zavadskaja, E. S., Rassamakin, B. M., Rogachov, V. A., Khairnasov, S. M., & Khominich, V. I. (2013). Experimental simulation of nanosatellites heat modes. Technology and Design in Electronic Equipment, (4), 27-30. Retrieved from http://www.tkea.com.ua/index.php/journal/article/view/TKEA2013.4.27
Section
Articles
Copyright (c) 2013 Zavadskaja E. S, Rassamakin B. M., Rogachov V. A., Khairnasov S. M., Khominich V. I.

This work is licensed under a Creative Commons Attribution 4.0 International License.