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Термовакуумные испытания оптико-электронных приборов космического аппарата МС-2-8

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...

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Bibliographic Details
Date:2008
Main Authors: Rassamakin, B. М., Rogachev, V. A., Khayrnasov, S. М., Khominich, V. I., Grеnyuk, I. Ye.
Format: Article
Language:Ukrainian
Published: PE "Politekhperiodika", Book and Journal Publishers 2008
Subjects:
тер­мо­ва­ку­ум­ные ис­пы­та­ния
теп­ло­об­мен в кос­мо­се
мик­ро­спут­ник
оп­ти­ко-элек­трон­ный при­бор
Online Access:https://www.tkea.com.ua/index.php/journal/article/view/TKEA2008.4.42
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Journal Title:Technology and design in electronic equipment

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Technology and design in electronic equipment
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Summary: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.

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