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Thermovacuum tests of optoelectronic devices of the spacecraft MС-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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Auteurs principaux: B. М. Rassamakin, V. A. Rogachev, S. М. Khayrnasov, V. I. Khominich, I. Ye. Grеnyuk
Format: Artigo
Langue:Inglês
Publié: Politekhperiodika 2008-08-01
Collection:Технологія та конструювання в електронній апаратурі
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Accès en ligne:https://tkea.com.ua/index.php/journal/article/view/745
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