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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Datum:2008
Hauptverfasser: Rassamakin, B. М., Rogachev, V. A., Khayrnasov, S. М., Khominich, V. I., Grеnyuk, I. Ye.
Format: Artikel
Sprache:Ukrainisch
Veröffentlicht: PE "Politekhperiodika", Book and Journal Publishers 2008
Schlagworte:
Online Zugang:https://www.tkea.com.ua/index.php/journal/article/view/TKEA2008.4.42
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Назва журналу:Technology and design in electronic equipment

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Technology and design in electronic equipment
Beschreibung
Zusammenfassung: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.