Parylene-based active micro space radiator with thermal contact switch
Thermal management is crucial for highly functional spacecrafts exposed to large fluctuations of internal heat dissipation and/or thermal boundary conditions. Since thermal radiation is the only means for heat removal, effective control of radiation is required for advanced space missions. In the pr...
Gespeichert in:
| Veröffentlicht in: | Applied physics letters 2014-03, Vol.104 (9) |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | 9 |
| container_start_page | |
| container_title | Applied physics letters |
| container_volume | 104 |
| creator | Ueno, Ai Suzuki, Yuji |
| description | Thermal management is crucial for highly functional spacecrafts exposed to large fluctuations of internal heat dissipation and/or thermal boundary conditions. Since thermal radiation is the only means for heat removal, effective control of radiation is required for advanced space missions. In the present study, a MEMS (Micro Electro Mechanical Systems) active radiator using the contact resistance change has been proposed. Unlike previous bulky thermal louvers/shutters, higher fill factor can be accomplished with an array of electrostatically driven micro diaphragms suspended with polymer tethers. With an early prototype developed with parylene MEMS technologies, radiation heat flux enhancement up to 42% has been achieved. |
| doi_str_mv | 10.1063/1.4867699 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_osti_</sourceid><recordid>TN_cdi_osti_scitechconnect_22283039</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2127685039</sourcerecordid><originalsourceid>FETCH-LOGICAL-c285t-bb37863587d1c511ae2058828b493966f522e162191ecdfaf9174c6991a833d33</originalsourceid><addsrcrecordid>eNpFkMFKAzEQhoMoWKsH3yDgycPWTKbJJkcptgoFPeg5ZLNZNqXdrUmq-PZGWvA0zPAx_P9HyC2wGTCJDzCbK1lLrc_IBFhdVwigzsmEMYaV1AIuyVVKm7IKjjghyzcbf7Z-8FVjk2-pdTl8eboLLo407a3zNNo22DxG-h1yT3Pv485uqRuHXGCaytX11-Sis9vkb05zSj6WT--L52r9unpZPK4rx5XIVdNgrSQKVbfgBID1nAmluGrmGrWUneDcg-Sgwbu2s52Geu5KG7AKsUWckrvj3zHlYJIL2bu-RBm8y4ZzrpCh_qf2cfw8-JTNZjzEoQQzHHgtlThS90eqVE0p-s7sY9gVHQaY-ZNpwJxk4i9yQ2QR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2127685039</pqid></control><display><type>article</type><title>Parylene-based active micro space radiator with thermal contact switch</title><source>American Institute of Physics (AIP) Journals</source><source>Alma/SFX Local Collection</source><creator>Ueno, Ai ; Suzuki, Yuji</creator><creatorcontrib>Ueno, Ai ; Suzuki, Yuji</creatorcontrib><description>Thermal management is crucial for highly functional spacecrafts exposed to large fluctuations of internal heat dissipation and/or thermal boundary conditions. Since thermal radiation is the only means for heat removal, effective control of radiation is required for advanced space missions. In the present study, a MEMS (Micro Electro Mechanical Systems) active radiator using the contact resistance change has been proposed. Unlike previous bulky thermal louvers/shutters, higher fill factor can be accomplished with an array of electrostatically driven micro diaphragms suspended with polymer tethers. With an early prototype developed with parylene MEMS technologies, radiation heat flux enhancement up to 42% has been achieved.</description><identifier>ISSN: 0003-6951</identifier><identifier>EISSN: 1077-3118</identifier><identifier>DOI: 10.1063/1.4867699</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Applied physics ; BOUNDARY CONDITIONS ; CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY ; Contact resistance ; Diaphragms ; ELECTROMECHANICS ; ENERGY LOSSES ; ENGINEERING ; FILL FACTORS ; FLUCTUATIONS ; HEAT FLUX ; HEAT TRANSFER ; Louvers ; Mechanical systems ; MICROSTRUCTURE ; ORGANIC POLYMERS ; RADIATORS ; Shutters ; Space missions ; SWITCHES ; Tethers ; THERMAL DIFFUSIVITY ; THERMAL EFFLUENTS ; Thermal management ; THERMAL RADIATION ; Variation</subject><ispartof>Applied physics letters, 2014-03, Vol.104 (9)</ispartof><rights>2014 AIP Publishing LLC.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c285t-bb37863587d1c511ae2058828b493966f522e162191ecdfaf9174c6991a833d33</citedby><cites>FETCH-LOGICAL-c285t-bb37863587d1c511ae2058828b493966f522e162191ecdfaf9174c6991a833d33</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://www.osti.gov/biblio/22283039$$D View this record in Osti.gov$$Hfree_for_read</backlink></links><search><creatorcontrib>Ueno, Ai</creatorcontrib><creatorcontrib>Suzuki, Yuji</creatorcontrib><title>Parylene-based active micro space radiator with thermal contact switch</title><title>Applied physics letters</title><description>Thermal management is crucial for highly functional spacecrafts exposed to large fluctuations of internal heat dissipation and/or thermal boundary conditions. Since thermal radiation is the only means for heat removal, effective control of radiation is required for advanced space missions. In the present study, a MEMS (Micro Electro Mechanical Systems) active radiator using the contact resistance change has been proposed. Unlike previous bulky thermal louvers/shutters, higher fill factor can be accomplished with an array of electrostatically driven micro diaphragms suspended with polymer tethers. With an early prototype developed with parylene MEMS technologies, radiation heat flux enhancement up to 42% has been achieved.</description><subject>Applied physics</subject><subject>BOUNDARY CONDITIONS</subject><subject>CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY</subject><subject>Contact resistance</subject><subject>Diaphragms</subject><subject>ELECTROMECHANICS</subject><subject>ENERGY LOSSES</subject><subject>ENGINEERING</subject><subject>FILL FACTORS</subject><subject>FLUCTUATIONS</subject><subject>HEAT FLUX</subject><subject>HEAT TRANSFER</subject><subject>Louvers</subject><subject>Mechanical systems</subject><subject>MICROSTRUCTURE</subject><subject>ORGANIC POLYMERS</subject><subject>RADIATORS</subject><subject>Shutters</subject><subject>Space missions</subject><subject>SWITCHES</subject><subject>Tethers</subject><subject>THERMAL DIFFUSIVITY</subject><subject>THERMAL EFFLUENTS</subject><subject>Thermal management</subject><subject>THERMAL RADIATION</subject><subject>Variation</subject><issn>0003-6951</issn><issn>1077-3118</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNpFkMFKAzEQhoMoWKsH3yDgycPWTKbJJkcptgoFPeg5ZLNZNqXdrUmq-PZGWvA0zPAx_P9HyC2wGTCJDzCbK1lLrc_IBFhdVwigzsmEMYaV1AIuyVVKm7IKjjghyzcbf7Z-8FVjk2-pdTl8eboLLo407a3zNNo22DxG-h1yT3Pv485uqRuHXGCaytX11-Sis9vkb05zSj6WT--L52r9unpZPK4rx5XIVdNgrSQKVbfgBID1nAmluGrmGrWUneDcg-Sgwbu2s52Geu5KG7AKsUWckrvj3zHlYJIL2bu-RBm8y4ZzrpCh_qf2cfw8-JTNZjzEoQQzHHgtlThS90eqVE0p-s7sY9gVHQaY-ZNpwJxk4i9yQ2QR</recordid><startdate>20140303</startdate><enddate>20140303</enddate><creator>Ueno, Ai</creator><creator>Suzuki, Yuji</creator><general>American Institute of Physics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>OTOTI</scope></search><sort><creationdate>20140303</creationdate><title>Parylene-based active micro space radiator with thermal contact switch</title><author>Ueno, Ai ; Suzuki, Yuji</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c285t-bb37863587d1c511ae2058828b493966f522e162191ecdfaf9174c6991a833d33</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Applied physics</topic><topic>BOUNDARY CONDITIONS</topic><topic>CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY</topic><topic>Contact resistance</topic><topic>Diaphragms</topic><topic>ELECTROMECHANICS</topic><topic>ENERGY LOSSES</topic><topic>ENGINEERING</topic><topic>FILL FACTORS</topic><topic>FLUCTUATIONS</topic><topic>HEAT FLUX</topic><topic>HEAT TRANSFER</topic><topic>Louvers</topic><topic>Mechanical systems</topic><topic>MICROSTRUCTURE</topic><topic>ORGANIC POLYMERS</topic><topic>RADIATORS</topic><topic>Shutters</topic><topic>Space missions</topic><topic>SWITCHES</topic><topic>Tethers</topic><topic>THERMAL DIFFUSIVITY</topic><topic>THERMAL EFFLUENTS</topic><topic>Thermal management</topic><topic>THERMAL RADIATION</topic><topic>Variation</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ueno, Ai</creatorcontrib><creatorcontrib>Suzuki, Yuji</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>OSTI.GOV</collection><jtitle>Applied physics letters</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ueno, Ai</au><au>Suzuki, Yuji</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Parylene-based active micro space radiator with thermal contact switch</atitle><jtitle>Applied physics letters</jtitle><date>2014-03-03</date><risdate>2014</risdate><volume>104</volume><issue>9</issue><issn>0003-6951</issn><eissn>1077-3118</eissn><abstract>Thermal management is crucial for highly functional spacecrafts exposed to large fluctuations of internal heat dissipation and/or thermal boundary conditions. Since thermal radiation is the only means for heat removal, effective control of radiation is required for advanced space missions. In the present study, a MEMS (Micro Electro Mechanical Systems) active radiator using the contact resistance change has been proposed. Unlike previous bulky thermal louvers/shutters, higher fill factor can be accomplished with an array of electrostatically driven micro diaphragms suspended with polymer tethers. With an early prototype developed with parylene MEMS technologies, radiation heat flux enhancement up to 42% has been achieved.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/1.4867699</doi></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0003-6951 |
| ispartof | Applied physics letters, 2014-03, Vol.104 (9) |
| issn | 0003-6951 1077-3118 |
| language | eng |
| recordid | cdi_osti_scitechconnect_22283039 |
| source | American Institute of Physics (AIP) Journals; Alma/SFX Local Collection |
| subjects | Applied physics BOUNDARY CONDITIONS CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY Contact resistance Diaphragms ELECTROMECHANICS ENERGY LOSSES ENGINEERING FILL FACTORS FLUCTUATIONS HEAT FLUX HEAT TRANSFER Louvers Mechanical systems MICROSTRUCTURE ORGANIC POLYMERS RADIATORS Shutters Space missions SWITCHES Tethers THERMAL DIFFUSIVITY THERMAL EFFLUENTS Thermal management THERMAL RADIATION Variation |
| title | Parylene-based active micro space radiator with thermal contact switch |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T18%3A28%3A35IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_osti_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Parylene-based%20active%20micro%20space%20radiator%20with%20thermal%20contact%20switch&rft.jtitle=Applied%20physics%20letters&rft.au=Ueno,%20Ai&rft.date=2014-03-03&rft.volume=104&rft.issue=9&rft.issn=0003-6951&rft.eissn=1077-3118&rft_id=info:doi/10.1063/1.4867699&rft_dat=%3Cproquest_osti_%3E2127685039%3C/proquest_osti_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2127685039&rft_id=info:pmid/&rfr_iscdi=true |