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Measurement of mechanical properties of electronic materials at temperatures down to 4.2 K
Authors:M Fink  Th Fabing  M Scheerer  E Semerad  B Dunn
Affiliation:1. ARC Seibersdorf Research GmbH, 2444 Seibersdorf, Austria;2. ESA/ESTEC, 2200 AG Noordwijk, The Netherlands;1. School of Electronic and Information Engineering, South China University of Technology, Guangzhou 510641, China;2. College of Electronic Engineering, South China Agriculture University, Guangzhou 510642, China;3. College of Automation, Zhongkai University of Agriculture and Engineering, Guangzhou 510225, China;1. Department of Mechanical and Materials Engineering, Queen’s University, Kingston, ON, Canada K7L 3N6;2. Material Science Division, Argonne National Laboratory, Argonne, IL 60439, USA;1. Department of Naval Architecture and Ocean Engineering, Pusan National University, 30, Jangjeon-Dong, Geumjeong-Gu, Busan 609-735, Republic of Korea;2. Department of Extreme Energy Systems, Korea Institute of Machinery and Materials, Daejeon 305-343, Republic of Korea
Abstract:Operating temperatures of spacecraft components in the ‘subzero’ range are encountered during solar eclipse periods or when voyaging on deep-space missions. Moreover some spacecraft instruments or parts of them, e.g. sensors, have to be cooled to obtain an improved performance, e.g. in spacecraft missions like the infrared space observatory (ISO) and CryoSat. Materials utilized in the assembly of electronic circuits can be subjected to mechanical loading at cryogenic temperatures. Semerad E, Scholze P, Schmidt M, Wendrinsky W. Effect of new cleaning liquids on electronic materials and parts. ESA metallurgy report no. 3275; January 2002, 1]].Within the present work the mechanical properties of electronic materials at cryogenic temperatures down to liquid helium temperature were analysed. Specifically the tensile properties of solders (63Sn37Pb, 62Sn36Pb2Ag, 60Sn40Pb, 96Sn4Ag, 50In50Pb, 70Pb30In, 96.8Pb1.5Ag1.7Sn, 96.5Sn3Ag0.5Cu), PC boards (MLB polyimide glass fibre, MLB epoxy glass fibre, MLB Thermount), conformal coatings (Arathane 5750, Sylgard 184, Scotchcast 280, Solithane 113, CV-1144-0, Mapsil 213, Conathane EN4/EN11) as well as OFE Cu were characterised at room temperature, at liquid nitrogen and at liquid helium temperature by tensile tests.The fracture surface of tested samples was examined by means of optical microscope and if necessary with scanning electron microscope.
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