Зображення обкладинки

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...

Повний опис

Збережено в:
Бібліографічні деталі
Дата:2008
Автори: Rassamakin, B. М., Rogachev, V. A., Khayrnasov, S. М., Khominich, V. I., Grеnyuk, I. Ye.
Формат: Стаття
Мова:Українська
Опубліковано: PE "Politekhperiodika", Book and Journal Publishers 2008
Теми:
тер­мо­ва­ку­ум­ные ис­пы­та­ния
теп­ло­об­мен в кос­мо­се
мик­ро­спут­ник
оп­ти­ко-элек­трон­ный при­бор
Онлайн доступ:https://www.tkea.com.ua/index.php/journal/article/view/TKEA2008.4.42
Теги: Додати тег
Немає тегів, Будьте першим, хто поставить тег для цього запису!
Назва журналу:Technology and design in electronic equipment

Репозитарії

Technology and design in electronic equipment
Опис
Резюме: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.

Схожі ресурси