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Investigation on the thermal properties of carbon fibres with silica-based aerogel composites
In this research, thermal protection systems of space hardware have prompted the development and study of silica aerogel composites bonded with a variety of Carbon fibres. Carbon fibres were woven into a matrix of tetra ethoxy silane (Ts) and vinyl tri-methoxy silane (Vs) to create these composites....
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Published in: | Journal of physics. Conference series 2023-10, Vol.2603 (1), p.12038 |
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creator | Ponnusamy, Prasanth Girisha, L Balamurugan, S Benham, A Vivek, R Loganathan, Ganesh Babu Girimurugan, R |
description | In this research, thermal protection systems of space hardware have prompted the development and study of silica aerogel composites bonded with a variety of Carbon fibres. Carbon fibres were woven into a matrix of tetra ethoxy silane (Ts) and vinyl tri-methoxy silane (Vs) to create these composites. Many different composites were developed, each with its own set of characteristics and capabilities because to the wide range of fibres used. The measured bulk density values were often relatively low, with the lowest recorded value being only 180 kg m
−3
. The thermal conductivity was reduced to below 30 mW m
−1
K
−1
and the stability was maintained up to 600°C. Nanocomposites consisting of longer fibres containing meta-Carbons are superior insulators, while short-fiber composites are stiffer and have lower thermal conductivities. The aerogel composites compliance with Space conditions was evaluated using standard Space materials qualification procedures like thermal cycling and outgassing, proving their fitness for use in this context. |
doi_str_mv | 10.1088/1742-6596/2603/1/012038 |
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−3
. The thermal conductivity was reduced to below 30 mW m
−1
K
−1
and the stability was maintained up to 600°C. Nanocomposites consisting of longer fibres containing meta-Carbons are superior insulators, while short-fiber composites are stiffer and have lower thermal conductivities. The aerogel composites compliance with Space conditions was evaluated using standard Space materials qualification procedures like thermal cycling and outgassing, proving their fitness for use in this context.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/2603/1/012038</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aerogel composites ; Bulk density ; Carbon ; Carbon fibers ; Fiber composites ; Insulators ; Nanocomposites ; Outgassing ; Physics ; Silanes ; Silica aerogels ; Space equipment ; Thermal conductivities ; Thermal conductivity ; Thermal cycling ; Thermal protection ; Thermodynamic properties ; Vinyltrimethoxysilane</subject><ispartof>Journal of physics. Conference series, 2023-10, Vol.2603 (1), p.12038</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>Published under licence by IOP Publishing Ltd. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c2748-ebf1b3756a469775e0772b64c2e5dc0e11383f65ab2b6202f458ae2b1a55c2913</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.proquest.com/docview/2888639820?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,777,781,25734,27905,27906,36993,44571</link.rule.ids></links><search><creatorcontrib>Ponnusamy, Prasanth</creatorcontrib><creatorcontrib>Girisha, L</creatorcontrib><creatorcontrib>Balamurugan, S</creatorcontrib><creatorcontrib>Benham, A</creatorcontrib><creatorcontrib>Vivek, R</creatorcontrib><creatorcontrib>Loganathan, Ganesh Babu</creatorcontrib><creatorcontrib>Girimurugan, R</creatorcontrib><title>Investigation on the thermal properties of carbon fibres with silica-based aerogel composites</title><title>Journal of physics. Conference series</title><addtitle>J. Phys.: Conf. Ser</addtitle><description>In this research, thermal protection systems of space hardware have prompted the development and study of silica aerogel composites bonded with a variety of Carbon fibres. Carbon fibres were woven into a matrix of tetra ethoxy silane (Ts) and vinyl tri-methoxy silane (Vs) to create these composites. Many different composites were developed, each with its own set of characteristics and capabilities because to the wide range of fibres used. The measured bulk density values were often relatively low, with the lowest recorded value being only 180 kg m
−3
. The thermal conductivity was reduced to below 30 mW m
−1
K
−1
and the stability was maintained up to 600°C. Nanocomposites consisting of longer fibres containing meta-Carbons are superior insulators, while short-fiber composites are stiffer and have lower thermal conductivities. The aerogel composites compliance with Space conditions was evaluated using standard Space materials qualification procedures like thermal cycling and outgassing, proving their fitness for use in this context.</description><subject>Aerogel composites</subject><subject>Bulk density</subject><subject>Carbon</subject><subject>Carbon fibers</subject><subject>Fiber composites</subject><subject>Insulators</subject><subject>Nanocomposites</subject><subject>Outgassing</subject><subject>Physics</subject><subject>Silanes</subject><subject>Silica aerogels</subject><subject>Space equipment</subject><subject>Thermal conductivities</subject><subject>Thermal conductivity</subject><subject>Thermal cycling</subject><subject>Thermal protection</subject><subject>Thermodynamic properties</subject><subject>Vinyltrimethoxysilane</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><recordid>eNqFkFtLwzAUgIMoOKe_wYJvQm0uzWWPMrxMBgrqo4QkS7aMbqlJp_jvTakogmBISDj5zjnJB8ApghcIClEhXuOS0QmrMIOkQhVEGBKxB0bfN_vfZyEOwVFKawhJHnwEXmbbN5s6v1SdD9siz25l-xU3qinaGFobO29TEVxhVNQZcF7HHHj33apIvvFGlVoluyiUjWFpm8KETRuS72w6BgdONcmefO1j8Hx99TS9Lef3N7Pp5bw0mNeitNohTThlqmYTzqmFnGPNaoMtXRhoESKCOEaVzlEMsaupUBZrpCg1eILIGJwNdfODX3f5P3IddnGbW0oshGBkIrKTMeADZWJIKVon2-g3Kn5IBGXvUvaWZG9M9i4lkoPLnHk-ZPrQ_pS-e5g-_gZlu3AZJn_A_7X4BCPlg_8</recordid><startdate>20231001</startdate><enddate>20231001</enddate><creator>Ponnusamy, Prasanth</creator><creator>Girisha, L</creator><creator>Balamurugan, S</creator><creator>Benham, A</creator><creator>Vivek, R</creator><creator>Loganathan, Ganesh Babu</creator><creator>Girimurugan, R</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope></search><sort><creationdate>20231001</creationdate><title>Investigation on the thermal properties of carbon fibres with silica-based aerogel composites</title><author>Ponnusamy, Prasanth ; 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−3
. The thermal conductivity was reduced to below 30 mW m
−1
K
−1
and the stability was maintained up to 600°C. Nanocomposites consisting of longer fibres containing meta-Carbons are superior insulators, while short-fiber composites are stiffer and have lower thermal conductivities. The aerogel composites compliance with Space conditions was evaluated using standard Space materials qualification procedures like thermal cycling and outgassing, proving their fitness for use in this context.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/2603/1/012038</doi><tpages>13</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aerogel composites Bulk density Carbon Carbon fibers Fiber composites Insulators Nanocomposites Outgassing Physics Silanes Silica aerogels Space equipment Thermal conductivities Thermal conductivity Thermal cycling Thermal protection Thermodynamic properties Vinyltrimethoxysilane |
title | Investigation on the thermal properties of carbon fibres with silica-based aerogel composites |
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