DocumentCode :
631258
Title :
Thermal vacuum cycling test philosophy of an indigenous earth observation satellite
Author :
Omur, Cem ; Uygur, A. Bilge ; Isik, H. Gurguc ; Akin, David
Author_Institution :
Space Syst., Turkish Aerosp. Ind. Inc., Ankara, Turkey
fYear :
2013
fDate :
12-14 June 2013
Firstpage :
537
Lastpage :
540
Abstract :
Satellites are subjected to extensive (ground level) environmental testing before launch to ensure successful launch and on-orbit operation. While there exists three primary environmental tests i.e., thermal, structural and electromagnetic interference/compatibility (EMI/EMC), the focus of this paper is on the thermal vacuum test applied to the flight model (FM) of an indigenous electro-optic satellite project carried out in Turkey.
Keywords :
Earth orbit; aerospace testing; artificial satellites; electromagnetic compatibility; electromagnetic interference; EMI-EMC; FM; electromagnetic interference-compatibility; extensive environmental testing; flight model; ground level environmental testing; indigenous Earth observation satellite; indigenous electro-optic satellite project; on-orbit operation; primary environmental tests; structural interference-compatibility; thermal interference-compatibility; thermal vacuum cycling test philosophy; Frequency modulation; Heating; Satellite broadcasting; Satellites; Temperature distribution; Testing; Uncertainty; Acceptance Level Tests; Thermal Vacuum Chamber; Thermal Vacuum Cycling Test;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2013 6th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4673-6395-2
Type :
conf
DOI :
10.1109/RAST.2013.6581268
Filename :
6581268
Link To Document :
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