Modeling Hydrogen Chloride and Aluminum Surface Interactions for Spacecraft Fire Safety Applications
Experiments and modeling were performed to determine the surface kinetics of gaseous hydrogen chloride (HCl) with aluminum surfaces subjected to various treatments. HCl and other acid gases are a spacecraft fire safety concern because they are commonly found in products from electrical wire pyrolysi...
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Veröffentlicht in: | Journal of spacecraft and rockets 2020-03, Vol.57 (2), p.217-224 |
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description | Experiments and modeling were performed to determine the surface kinetics of gaseous hydrogen chloride (HCl) with aluminum surfaces subjected to various treatments. HCl and other acid gases are a spacecraft fire safety concern because they are commonly found in products from electrical wire pyrolysis. Three types of aluminum surfaces were considered: surface with chromate conversion coating (iridite), anodized, and untreated. A test cell made of polytetrafluoroethylene was used to measure the difference in the HCl concentration from the inlet to the outlet. A simple one-step global surface reaction model that accounts for active surface sites was proposed. The kinetic constants were calibrated using the measured data. The calibrated model was validated against experiments with different flow rates and HCl inlet concentrations. The results showed that anodized aluminum had the most HCl uptake, followed by the iridite, and then the untreated aluminum. The amount of HCl uptake appeared to correlate well with the thickness of the oxide layer on aluminum. The relevance of these findings is discussed with respect to the design of large-scale fire safety experiments in space and various fire safety application scenarios. |
doi_str_mv | 10.2514/1.A34621 |
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HCl and other acid gases are a spacecraft fire safety concern because they are commonly found in products from electrical wire pyrolysis. Three types of aluminum surfaces were considered: surface with chromate conversion coating (iridite), anodized, and untreated. A test cell made of polytetrafluoroethylene was used to measure the difference in the HCl concentration from the inlet to the outlet. A simple one-step global surface reaction model that accounts for active surface sites was proposed. The kinetic constants were calibrated using the measured data. The calibrated model was validated against experiments with different flow rates and HCl inlet concentrations. The results showed that anodized aluminum had the most HCl uptake, followed by the iridite, and then the untreated aluminum. The amount of HCl uptake appeared to correlate well with the thickness of the oxide layer on aluminum. The relevance of these findings is discussed with respect to the design of large-scale fire safety experiments in space and various fire safety application scenarios.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A34621</identifier><language>eng</language><publisher>RESTON: American Institute of Aeronautics and Astronautics</publisher><subject>Aluminum ; Chromating ; Conversion coating ; Engineering ; Engineering, Aerospace ; Experiments ; Fire protection ; Fire safety ; Flow velocity ; Hydrochloric acid ; Hydrogen chloride ; Modelling ; Polytetrafluoroethylene ; Product safety ; Pyrolysis ; Reaction kinetics ; Science & Technology ; Spacecraft ; Surface kinetics ; Surface reactions ; Technology ; Thickness</subject><ispartof>Journal of spacecraft and rockets, 2020-03, Vol.57 (2), p.217-224</ispartof><rights>This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-6794 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>true</woscitedreferencessubscribed><woscitedreferencescount>2</woscitedreferencescount><woscitedreferencesoriginalsourcerecordid>wos000521267100002</woscitedreferencesoriginalsourcerecordid><citedby>FETCH-LOGICAL-a356t-207c474f752938bdaf98c173a326d58ca6173feed5104ee806914284f5d190743</citedby><cites>FETCH-LOGICAL-a356t-207c474f752938bdaf98c173a326d58ca6173feed5104ee806914284f5d190743</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,781,785,27929,27930,28253</link.rule.ids></links><search><creatorcontrib>Niehaus, Justin E</creatorcontrib><creatorcontrib>Gokoglu, Suleyman A</creatorcontrib><creatorcontrib>Berger, Gordon</creatorcontrib><creatorcontrib>Easton, John</creatorcontrib><creatorcontrib>Mazumder, Sandip</creatorcontrib><title>Modeling Hydrogen Chloride and Aluminum Surface Interactions for Spacecraft Fire Safety Applications</title><title>Journal of spacecraft and rockets</title><addtitle>J SPACECRAFT ROCKETS</addtitle><description>Experiments and modeling were performed to determine the surface kinetics of gaseous hydrogen chloride (HCl) with aluminum surfaces subjected to various treatments. HCl and other acid gases are a spacecraft fire safety concern because they are commonly found in products from electrical wire pyrolysis. Three types of aluminum surfaces were considered: surface with chromate conversion coating (iridite), anodized, and untreated. A test cell made of polytetrafluoroethylene was used to measure the difference in the HCl concentration from the inlet to the outlet. A simple one-step global surface reaction model that accounts for active surface sites was proposed. The kinetic constants were calibrated using the measured data. The calibrated model was validated against experiments with different flow rates and HCl inlet concentrations. The results showed that anodized aluminum had the most HCl uptake, followed by the iridite, and then the untreated aluminum. The amount of HCl uptake appeared to correlate well with the thickness of the oxide layer on aluminum. The relevance of these findings is discussed with respect to the design of large-scale fire safety experiments in space and various fire safety application scenarios.</description><subject>Aluminum</subject><subject>Chromating</subject><subject>Conversion coating</subject><subject>Engineering</subject><subject>Engineering, Aerospace</subject><subject>Experiments</subject><subject>Fire protection</subject><subject>Fire safety</subject><subject>Flow velocity</subject><subject>Hydrochloric acid</subject><subject>Hydrogen chloride</subject><subject>Modelling</subject><subject>Polytetrafluoroethylene</subject><subject>Product safety</subject><subject>Pyrolysis</subject><subject>Reaction kinetics</subject><subject>Science & Technology</subject><subject>Spacecraft</subject><subject>Surface kinetics</subject><subject>Surface reactions</subject><subject>Technology</subject><subject>Thickness</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>AOWDO</sourceid><recordid>eNqNkEtL7TAUhYMoeHyAPyEggiDVvNMOD-X6AMXB0XGJyY5GepKatlzOv7da0YETR_vBt_ZeLISOKDlnkooLer7kQjG6hRZUcl4oXYlttCCEsUIoSXbRXt-_EkJVqaoFcnfJQRviM77euJyeIeL6pU05OMAmOrxsx3WI4xqvxuyNBXwTB8jGDiHFHvuU8aqb1jYbP-DLkAGvjIdhg5dd1wZrPrkDtONN28PhV91Hj5f_Hurr4vb-6qZe3haGSzUUjGgrtPBasoqXT874qrRUc8OZcrK0Rk2DB3CSEgFQElVRwUrhpaMV0YLvo-P5bpfT2wj90LymMcfpZcO41popVbKJOp0pm1PfZ_BNl8Pa5E1DSfORYUObOcMJPZvR__CUfG8DRAvfOCFEMsqUplNHPg6Xf6frMHyGU6cxDpP0ZJaaYMyP61-G3gFF8o7N</recordid><startdate>20200301</startdate><enddate>20200301</enddate><creator>Niehaus, Justin E</creator><creator>Gokoglu, Suleyman A</creator><creator>Berger, Gordon</creator><creator>Easton, John</creator><creator>Mazumder, Sandip</creator><general>American Institute of Aeronautics and Astronautics</general><general>Amer Inst Aeronautics Astronautics</general><scope>95M</scope><scope>ABMOY</scope><scope>AOWDO</scope><scope>BLEPL</scope><scope>DTL</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20200301</creationdate><title>Modeling Hydrogen Chloride and Aluminum Surface Interactions for Spacecraft Fire Safety Applications</title><author>Niehaus, Justin E ; Gokoglu, Suleyman A ; Berger, Gordon ; Easton, John ; Mazumder, Sandip</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a356t-207c474f752938bdaf98c173a326d58ca6173feed5104ee806914284f5d190743</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aluminum</topic><topic>Chromating</topic><topic>Conversion coating</topic><topic>Engineering</topic><topic>Engineering, Aerospace</topic><topic>Experiments</topic><topic>Fire protection</topic><topic>Fire safety</topic><topic>Flow velocity</topic><topic>Hydrochloric acid</topic><topic>Hydrogen chloride</topic><topic>Modelling</topic><topic>Polytetrafluoroethylene</topic><topic>Product safety</topic><topic>Pyrolysis</topic><topic>Reaction kinetics</topic><topic>Science & Technology</topic><topic>Spacecraft</topic><topic>Surface kinetics</topic><topic>Surface reactions</topic><topic>Technology</topic><topic>Thickness</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Niehaus, Justin E</creatorcontrib><creatorcontrib>Gokoglu, Suleyman A</creatorcontrib><creatorcontrib>Berger, Gordon</creatorcontrib><creatorcontrib>Easton, John</creatorcontrib><creatorcontrib>Mazumder, Sandip</creatorcontrib><collection>Conference Proceedings Citation Index - Science (CPCI-S)</collection><collection>Conference Proceedings Citation Index - Science (CPCI-S) 2020</collection><collection>Web of Science - Science Citation Index Expanded - 2020</collection><collection>Web of Science Core Collection</collection><collection>Science Citation Index Expanded</collection><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><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Niehaus, Justin E</au><au>Gokoglu, Suleyman A</au><au>Berger, Gordon</au><au>Easton, John</au><au>Mazumder, Sandip</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Modeling Hydrogen Chloride and Aluminum Surface Interactions for Spacecraft Fire Safety Applications</atitle><jtitle>Journal of spacecraft and rockets</jtitle><stitle>J SPACECRAFT ROCKETS</stitle><date>2020-03-01</date><risdate>2020</risdate><volume>57</volume><issue>2</issue><spage>217</spage><epage>224</epage><pages>217-224</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>Experiments and modeling were performed to determine the surface kinetics of gaseous hydrogen chloride (HCl) with aluminum surfaces subjected to various treatments. HCl and other acid gases are a spacecraft fire safety concern because they are commonly found in products from electrical wire pyrolysis. Three types of aluminum surfaces were considered: surface with chromate conversion coating (iridite), anodized, and untreated. A test cell made of polytetrafluoroethylene was used to measure the difference in the HCl concentration from the inlet to the outlet. A simple one-step global surface reaction model that accounts for active surface sites was proposed. The kinetic constants were calibrated using the measured data. The calibrated model was validated against experiments with different flow rates and HCl inlet concentrations. The results showed that anodized aluminum had the most HCl uptake, followed by the iridite, and then the untreated aluminum. The amount of HCl uptake appeared to correlate well with the thickness of the oxide layer on aluminum. The relevance of these findings is discussed with respect to the design of large-scale fire safety experiments in space and various fire safety application scenarios.</abstract><cop>RESTON</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.A34621</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aluminum Chromating Conversion coating Engineering Engineering, Aerospace Experiments Fire protection Fire safety Flow velocity Hydrochloric acid Hydrogen chloride Modelling Polytetrafluoroethylene Product safety Pyrolysis Reaction kinetics Science & Technology Spacecraft Surface kinetics Surface reactions Technology Thickness |
title | Modeling Hydrogen Chloride and Aluminum Surface Interactions for Spacecraft Fire Safety Applications |
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