{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/110605"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/110605","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Preliminary design of a high enthalpy plasma tunnel for atmospheric re-entry research","abstract":"The following thesis discusses the conceptual design of the Plasmatron One wind tunnel at the Center for Hypersonics and Entry Systems Studies (CHESS) at the University of Illinois at Urbana Champaign (UIUC). The centerpiece of the facility is an Inductively Coupled Plasma (ICP) torch capable of recreating flow conditions similar to what reentering spacecraft experience when passing through the atmosphere. The purpose of this facility is to experimentally study the physics of plasma flows, their interactions with a downstream sample of thermal protection material, and the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material performance characteristics. This thesis describes the preliminary design process and its respective considerations as well as the goals of the facility and how they were achieved through various design features.","abstract_html":"The following thesis discusses the conceptual design of the Plasmatron One wind tunnel at the Center for Hypersonics and Entry Systems Studies (CHESS) at the University of Illinois at Urbana Champaign (UIUC). The centerpiece of the facility is an Inductively Coupled Plasma (ICP) torch capable of recreating flow conditions similar to what reentering spacecraft experience when passing through the atmosphere. The purpose of this facility is to experimentally study the physics of plasma flows, their interactions with a downstream sample of thermal protection material, and the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material performance characteristics. This thesis describes the preliminary design process and its respective considerations as well as the goals of the facility and how they were achieved through various design features.","abstract_has_math":false,"creators":["Czop, Matthew Mark"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Panerai, Francesco"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2021,"date_issued":"2021-09-17T01:13:35Z","date_published":"2021-09-17T01:13:35Z","updated_at":"2026-07-22T22:24:52Z","subjects":["Atmospheric Re-entry","Inductively Coupled Plasma","Thermal Protection System","Material Testing"],"languages":["en"],"rights":["Copyright 2021 Matthew Czop"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"http://hdl.handle.net/2142/110605","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Panerai, Francesco"]},{"key":"dc:creator","label":"Author","values":["Czop, Matthew Mark"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2021-09-17T01:13:35Z","2021-04-30","2021-05"]},{"key":"dc:type","label":"Dc Type","values":["text","Thesis"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis"]},{"key":"thesis:degree_name","label":"Degree Name","values":["M.S."]},{"key":"thesis:institution_name","label":"Thesis Institution Name","values":["University of Illinois at Urbana-Champaign"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["Atmospheric Re-entry","Inductively Coupled Plasma","Thermal Protection System","Material Testing"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en"]},{"key":"dc:rights","label":"Dc Rights","values":["Copyright 2021 Matthew Czop"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["http://hdl.handle.net/2142/110605"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["The following thesis discusses the conceptual design of the Plasmatron One wind tunnel at the Center for Hypersonics and Entry Systems Studies (CHESS) at the University of Illinois at Urbana Champaign (UIUC). The centerpiece of the facility is an Inductively Coupled Plasma (ICP) torch capable of recreating flow conditions similar to what reentering spacecraft experience when passing through the atmosphere. The purpose of this facility is to experimentally study the physics of plasma flows, their interactions with a downstream sample of thermal protection material, and the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material performance characteristics. This thesis describes the preliminary design process and its respective considerations as well as the goals of the facility and how they were achieved through various design features.","Submission original under an indefinite embargo labeled 'Open Access'. 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The centerpiece of the facility is an Inductively Coupled Plasma (ICP) torch capable of recreating flow conditions similar to what reentering spacecraft experience when passing through the atmosphere. The purpose of this facility is to experimentally study the physics of plasma flows, their interactions with a downstream sample of thermal protection material, and the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material performance characteristics. This thesis describes the preliminary design process and its respective considerations as well as the goals of the facility and how they were achieved through various design features.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2021-09-16 without embargo terms","The student, Matthew Czop, accepted the attached license on 2021-04-30 at 10:18.","The student, Matthew Czop, submitted this Thesis for approval on 2021-04-30 at 10:37.","This Thesis was approved for publication on 2021-04-30 at 13:20.","DSpace SAF Submission Ingestion Package generated from Vireo submission #16622 on 2021-09-16 at 16:49:45","Made available in DSpace on 2021-09-17T01:13:35Z (GMT). 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