Thermovacuum tests of optoelectronic devices of the spacecraft MС-2-8

  • B. М. Rassamakin NTUU «Kiev politechnic university», Ukraine
  • V. A. Rogachev NTUU «Kiev politechnic university», Ukraine
  • S. М. Khayrnasov NTUU «Kiev politechnic university», Ukraine
  • V. I. Khominich Central Design Department «Arsenal», Kyiv, Ukraine
  • I. Ye. Grеnyuk Central Design Department «Arsenal», Kyiv, Ukraine
Keywords: thermal vacuum tests, heat transfer in space, micro satellite, optoelectronic device

Abstract

A description is given of the TВK-2.5 installation for thermovacuum testing of spacecraft and instruments intended for space applications. The results of thermovacuum tests of a thermal mock-up of the small spacecraft MС-2-8 with optoelectronic devices (OED) mounted on it, as well as with simulators of external and internal thermal radiation, are presented. The thermovacuum tests were carried out in order to determine the orbital reliability of the OED.

Published
2008-08-30
How to Cite
RassamakinB. М., Rogachev, V. A., KhayrnasovS. М., Khominich, V. I., & GrеnyukI. Y. (2008). Thermovacuum tests of optoelectronic devices of the spacecraft MС-2-8. Technology and Design in Electronic Equipment, (4), 42-46. Retrieved from https://tkea.com.ua/index.php/journal/article/view/TKEA2008.4.42
Issue
No. 4 (2008): Tekhnologiya i konstruirovanie v elektronnoi apparature
Section
Articles

Copyright (c) 2008 Rassamakin B. М., Rogachev V. A., Khayrnasov S. М., Khominich V. I., Grеnyuk I. Ye.

Creative Commons License

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