Operational thermal conditions of optoelectronic devices for МС-2-8 space vehicle

• Main Authors: Grеnyuk I. Ye., Khominich V. I., Rogachev V. A., Khayrnasov S. М., Rassamakin B. М.
• Format: Article
• Language: English
• Published: Politehperiodika 2008-08-01
• Series: Tekhnologiya i Konstruirovanie v Elektronnoi Apparature
• Subjects: thermal vacuum tests; heat transfer in space; micro satellite; optoelectronic device
• Online Access: http://www.tkea.com.ua/tkea/2008/4_2008/pdf/11.zip
• ISSN: 2225-5818

Description of ТВК-2.5 simulation plant for thermal vacuum tests on space applied equipment and devices are given. Thermal vacuum test results on thermal mock-up of МС-2-8 small space vehicle (SP) with mounted on-board optoelectronic devices (OED) and with simulators of external and internal thermal radiation are adduced. Thermal vacuum tests were carried out in order to ensure OED reliability in orbit.