Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment
The development of radiation resistant materials is an ongoing challenge for space industry. High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhe...
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creator | Planes, M Le Coz, C Soum, A Carlotti, S Rejsek-Riba, V Lewandowski, S Remaury, S Solé, S |
description | The development of radiation resistant materials is an ongoing challenge for space industry. High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhesive materials for satellites. Polydimethylsiloxanes show material exhaustion after long-term exposure to ultraviolet irradiation. Consequently, solutions are required to increase their thermo- and photostability under solar irradiation. Three different families of additives, namely ultraviolet absorbers, hindered amine light stabilizers, and a carbazole derivative are investigated. Those ultraviolet stabilizers were mixed with polydimethylsiloxane, then a cross-linking process was run by hydrosilylation. When ultraviolet absorbers could not be used due to a miscibility problem, addition of 0.5 wt % of bis(2,2,6,6-tetramethylpiperidin-4-yl)decanedioate (hindered amine light stabilizer 1) was shown to increase the thermal stability, measured by thermogravimetric analysis, from 360 to 395°C (Td5%). Using visible near-infrared spectroscopy and after 450 equivalent solar hours of ultraviolet irradiation, an average increase of 2.6% in the ultraviolet stability was also obtained in the wavelength range from 250 to 400 nm. A polydimethylsiloxane/dibromocarbazole 1.0 wt% did not improve the ultraviolet stability but exhibited a strong increase (about 100°C) of the degradation temperature of the polydimethylsiloxane. |
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High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhesive materials for satellites. Polydimethylsiloxanes show material exhaustion after long-term exposure to ultraviolet irradiation. Consequently, solutions are required to increase their thermo- and photostability under solar irradiation. Three different families of additives, namely ultraviolet absorbers, hindered amine light stabilizers, and a carbazole derivative are investigated. Those ultraviolet stabilizers were mixed with polydimethylsiloxane, then a cross-linking process was run by hydrosilylation. When ultraviolet absorbers could not be used due to a miscibility problem, addition of 0.5 wt % of bis(2,2,6,6-tetramethylpiperidin-4-yl)decanedioate (hindered amine light stabilizer 1) was shown to increase the thermal stability, measured by thermogravimetric analysis, from 360 to 395°C (Td5%). Using visible near-infrared spectroscopy and after 450 equivalent solar hours of ultraviolet irradiation, an average increase of 2.6% in the ultraviolet stability was also obtained in the wavelength range from 250 to 400 nm. A polydimethylsiloxane/dibromocarbazole 1.0 wt% did not improve the ultraviolet stability but exhibited a strong increase (about 100°C) of the degradation temperature of the polydimethylsiloxane.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A33484</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Absorbers ; Additives ; Amines ; Carbazoles ; Crosslinking ; Derivatives ; Electronic components ; Exhaustion ; Hydrosilylation ; Infrared analysis ; Infrared spectra ; Irradiation ; Miscibility ; Near infrared radiation ; Physics ; Polydimethylsiloxane ; Proton damage ; Radiation damage ; Radiation tolerance ; Silicone resins ; Space Physics ; Spacecraft ; Stability ; Stability analysis ; Thermal stability ; Thermogravimetric analysis ; Ultraviolet ; Ultraviolet radiation ; UV stabilizers</subject><ispartof>Journal of spacecraft and rockets, 2016-11, Vol.53 (6), p.1128-1133</ispartof><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request.</rights><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0022-4650 (print) or 1533-6794 (online) to initiate your request.</rights><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0022-4650 (print) or 1533-6794 (online) to initiate your request.</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a414t-2fd4bc59bc791370df12917b7da1c261395ca036fab6d0755392b7094928e863</citedby><cites>FETCH-LOGICAL-a414t-2fd4bc59bc791370df12917b7da1c261395ca036fab6d0755392b7094928e863</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,314,780,784,885,27924,27925</link.rule.ids><backlink>$$Uhttps://hal.science/hal-01487978$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Planes, M</creatorcontrib><creatorcontrib>Le Coz, C</creatorcontrib><creatorcontrib>Soum, A</creatorcontrib><creatorcontrib>Carlotti, S</creatorcontrib><creatorcontrib>Rejsek-Riba, V</creatorcontrib><creatorcontrib>Lewandowski, S</creatorcontrib><creatorcontrib>Remaury, S</creatorcontrib><creatorcontrib>Solé, S</creatorcontrib><title>Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment</title><title>Journal of spacecraft and rockets</title><description>The development of radiation resistant materials is an ongoing challenge for space industry. High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhesive materials for satellites. Polydimethylsiloxanes show material exhaustion after long-term exposure to ultraviolet irradiation. Consequently, solutions are required to increase their thermo- and photostability under solar irradiation. Three different families of additives, namely ultraviolet absorbers, hindered amine light stabilizers, and a carbazole derivative are investigated. Those ultraviolet stabilizers were mixed with polydimethylsiloxane, then a cross-linking process was run by hydrosilylation. When ultraviolet absorbers could not be used due to a miscibility problem, addition of 0.5 wt % of bis(2,2,6,6-tetramethylpiperidin-4-yl)decanedioate (hindered amine light stabilizer 1) was shown to increase the thermal stability, measured by thermogravimetric analysis, from 360 to 395°C (Td5%). Using visible near-infrared spectroscopy and after 450 equivalent solar hours of ultraviolet irradiation, an average increase of 2.6% in the ultraviolet stability was also obtained in the wavelength range from 250 to 400 nm. A polydimethylsiloxane/dibromocarbazole 1.0 wt% did not improve the ultraviolet stability but exhibited a strong increase (about 100°C) of the degradation temperature of the polydimethylsiloxane.</description><subject>Absorbers</subject><subject>Additives</subject><subject>Amines</subject><subject>Carbazoles</subject><subject>Crosslinking</subject><subject>Derivatives</subject><subject>Electronic components</subject><subject>Exhaustion</subject><subject>Hydrosilylation</subject><subject>Infrared analysis</subject><subject>Infrared spectra</subject><subject>Irradiation</subject><subject>Miscibility</subject><subject>Near infrared radiation</subject><subject>Physics</subject><subject>Polydimethylsiloxane</subject><subject>Proton damage</subject><subject>Radiation damage</subject><subject>Radiation tolerance</subject><subject>Silicone resins</subject><subject>Space Physics</subject><subject>Spacecraft</subject><subject>Stability</subject><subject>Stability analysis</subject><subject>Thermal stability</subject><subject>Thermogravimetric analysis</subject><subject>Ultraviolet</subject><subject>Ultraviolet radiation</subject><subject>UV stabilizers</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNp90VtLHDEUAOAgLbjVQn9CoBTah9Gc3PO4iFVhoYLb55CZybCRzMQm2cX59x3ZYosPfTpw-DhXhD4BuaAC-CVcrBnjmp-gFQjGGqkMf4dWhFDacCnIKfpQyiMhILU0K7S7T3Huw-jrbo4lxPTsJn-57vtQw8Hjh7lUPxY8pIy3O59HF7Gbevwz1uwOIUVf8UN1bYihzjhM-ManUl0NaXJ5xtfTIeQ0jX6q5-j94GLxH__EM7T9fr29um02P27urtabxnHgtaFDz9tOmLZTBpgi_QDUgGpV76CjEpgRnSNMDq6VPVFCMENbRQw3VHst2Rn6diy7c9E-5TAuY9jkgr1db-xLjgDXyih9gMV-PdqnnH7tfal2DKXzMS4nSPtiQWtOjOHCLPTzG_qY9nlaFrEUpFLSaEb-p0BLSTRTQv9t2-VUSvbD65xA7MsPLdjjDxf65UhdcO6fYm_db2w0mHA</recordid><startdate>20161101</startdate><enddate>20161101</enddate><creator>Planes, M</creator><creator>Le Coz, C</creator><creator>Soum, A</creator><creator>Carlotti, S</creator><creator>Rejsek-Riba, V</creator><creator>Lewandowski, S</creator><creator>Remaury, S</creator><creator>Solé, S</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>1XC</scope><scope>VOOES</scope></search><sort><creationdate>20161101</creationdate><title>Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment</title><author>Planes, M ; Le Coz, C ; Soum, A ; Carlotti, S ; Rejsek-Riba, V ; Lewandowski, S ; Remaury, S ; Solé, S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a414t-2fd4bc59bc791370df12917b7da1c261395ca036fab6d0755392b7094928e863</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Absorbers</topic><topic>Additives</topic><topic>Amines</topic><topic>Carbazoles</topic><topic>Crosslinking</topic><topic>Derivatives</topic><topic>Electronic components</topic><topic>Exhaustion</topic><topic>Hydrosilylation</topic><topic>Infrared analysis</topic><topic>Infrared spectra</topic><topic>Irradiation</topic><topic>Miscibility</topic><topic>Near infrared radiation</topic><topic>Physics</topic><topic>Polydimethylsiloxane</topic><topic>Proton damage</topic><topic>Radiation damage</topic><topic>Radiation tolerance</topic><topic>Silicone resins</topic><topic>Space Physics</topic><topic>Spacecraft</topic><topic>Stability</topic><topic>Stability analysis</topic><topic>Thermal stability</topic><topic>Thermogravimetric analysis</topic><topic>Ultraviolet</topic><topic>Ultraviolet radiation</topic><topic>UV stabilizers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Planes, M</creatorcontrib><creatorcontrib>Le Coz, C</creatorcontrib><creatorcontrib>Soum, A</creatorcontrib><creatorcontrib>Carlotti, S</creatorcontrib><creatorcontrib>Rejsek-Riba, V</creatorcontrib><creatorcontrib>Lewandowski, S</creatorcontrib><creatorcontrib>Remaury, S</creatorcontrib><creatorcontrib>Solé, S</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Planes, M</au><au>Le Coz, C</au><au>Soum, A</au><au>Carlotti, S</au><au>Rejsek-Riba, V</au><au>Lewandowski, S</au><au>Remaury, S</au><au>Solé, S</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2016-11-01</date><risdate>2016</risdate><volume>53</volume><issue>6</issue><spage>1128</spage><epage>1133</epage><pages>1128-1133</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The development of radiation resistant materials is an ongoing challenge for space industry. High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhesive materials for satellites. Polydimethylsiloxanes show material exhaustion after long-term exposure to ultraviolet irradiation. Consequently, solutions are required to increase their thermo- and photostability under solar irradiation. Three different families of additives, namely ultraviolet absorbers, hindered amine light stabilizers, and a carbazole derivative are investigated. Those ultraviolet stabilizers were mixed with polydimethylsiloxane, then a cross-linking process was run by hydrosilylation. When ultraviolet absorbers could not be used due to a miscibility problem, addition of 0.5 wt % of bis(2,2,6,6-tetramethylpiperidin-4-yl)decanedioate (hindered amine light stabilizer 1) was shown to increase the thermal stability, measured by thermogravimetric analysis, from 360 to 395°C (Td5%). Using visible near-infrared spectroscopy and after 450 equivalent solar hours of ultraviolet irradiation, an average increase of 2.6% in the ultraviolet stability was also obtained in the wavelength range from 250 to 400 nm. A polydimethylsiloxane/dibromocarbazole 1.0 wt% did not improve the ultraviolet stability but exhibited a strong increase (about 100°C) of the degradation temperature of the polydimethylsiloxane.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.A33484</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Absorbers Additives Amines Carbazoles Crosslinking Derivatives Electronic components Exhaustion Hydrosilylation Infrared analysis Infrared spectra Irradiation Miscibility Near infrared radiation Physics Polydimethylsiloxane Proton damage Radiation damage Radiation tolerance Silicone resins Space Physics Spacecraft Stability Stability analysis Thermal stability Thermogravimetric analysis Ultraviolet Ultraviolet radiation UV stabilizers |
title | Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment |
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