{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/110568"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/110568","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Power system sizing and analysis for electric aircraft conceptual design","abstract":"This thesis presents research into and development of a suggested methodology for the sizing of an electrical power generation, distribution, and propulsion system for electric airplanes at the conceptual design level. Considerations for machine type, energy storage technology, volume packaging, and modeling are discussed. The methodology is applied to a design study for a medium-altitude, long-endurance survey drone to demonstrate the process and results. Finally, future research topics in the electric aircraft design space are suggested, particularly the need for a dedicated tool for electric aircraft powertrain analysis.","abstract_html":"This thesis presents research into and development of a suggested methodology for the sizing of an electrical power generation, distribution, and propulsion system for electric airplanes at the conceptual design level. Considerations for machine type, energy storage technology, volume packaging, and modeling are discussed. The methodology is applied to a design study for a medium-altitude, long-endurance survey drone to demonstrate the process and results. Finally, future research topics in the electric aircraft design space are suggested, particularly the need for a dedicated tool for electric aircraft powertrain analysis.","abstract_has_math":false,"creators":["Reband, John"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Electrical & Computer Engr","degree_department":null,"school":null,"contributors":["Haran, Kiruba S"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2021,"date_issued":"2021-09-17T01:11:17Z","date_published":"2021-09-17T01:11:17Z","updated_at":"2026-07-22T22:24:52Z","subjects":["Electric Aircraft","Powertrain","Conceptual Design","Aircraft Conceptual Design"],"languages":["en"],"rights":["©2021 John Reband"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"http://hdl.handle.net/2142/110568","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Haran, Kiruba S"]},{"key":"dc:creator","label":"Author","values":["Reband, John"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2021-09-17T01:11:17Z","2021-04-27","2021-05"]},{"key":"dc:type","label":"Dc Type","values":["text","Thesis"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Electrical & Computer Engr"]},{"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":["Electric Aircraft","Powertrain","Conceptual Design","Aircraft Conceptual Design"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en"]},{"key":"dc:rights","label":"Dc Rights","values":["©2021 John Reband"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["http://hdl.handle.net/2142/110568"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["This thesis presents research into and development of a suggested methodology for the sizing of an electrical power generation, distribution, and propulsion system for electric airplanes at the conceptual design level. Considerations for machine type, energy storage technology, volume packaging, and modeling are discussed. The methodology is applied to a design study for a medium-altitude, long-endurance survey drone to demonstrate the process and results. Finally, future research topics in the electric aircraft design space are suggested, particularly the need for a dedicated tool for electric aircraft powertrain analysis.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2021-09-16 without embargo terms","The student, John Reband, accepted the attached license on 2021-04-23 at 15:45.","The student, John Reband, submitted this Thesis for approval on 2021-04-23 at 16:09.","This Thesis was approved for publication on 2021-04-27 at 09:07.","DSpace SAF Submission Ingestion Package generated from Vireo submission #16537 on 2021-09-16 at 16:47:30","Made available in DSpace on 2021-09-17T01:11:17Z (GMT). No. of bitstreams: 3 REBAND-THESIS-2021.pdf: 551747 bytes, checksum: e615e84f6c92ac5d84c38344f943bd41 (MD5) Reband_Thesis_04232021.zip: 576023 bytes, checksum: f2fafb733fd3185741bf2ebce9d7736b (MD5) LICENSE.txt: 4208 bytes, checksum: 561ec01cc3db715782895610b58d39fa (MD5) Previous issue date: 2021-04-27"]},{"key":"dc:format","label":"Dc Format","values":["application/pdf"]},{"key":"dc:title","label":"Title","values":["Power system sizing and analysis for electric aircraft conceptual design"]}]}],"canonical_facts":{"dc:contributor":["Haran, Kiruba S"],"dc:creator":["Reband, John"],"dc:date":["2021-09-17T01:11:17Z","2021-04-27","2021-05"],"dc:description":["This thesis presents research into and development of a suggested methodology for the sizing of an electrical power generation, distribution, and propulsion system for electric airplanes at the conceptual design level. Considerations for machine type, energy storage technology, volume packaging, and modeling are discussed. The methodology is applied to a design study for a medium-altitude, long-endurance survey drone to demonstrate the process and results. Finally, future research topics in the electric aircraft design space are suggested, particularly the need for a dedicated tool for electric aircraft powertrain analysis.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2021-09-16 without embargo terms","The student, John Reband, accepted the attached license on 2021-04-23 at 15:45.","The student, John Reband, submitted this Thesis for approval on 2021-04-23 at 16:09.","This Thesis was approved for publication on 2021-04-27 at 09:07.","DSpace SAF Submission Ingestion Package generated from Vireo submission #16537 on 2021-09-16 at 16:47:30","Made available in DSpace on 2021-09-17T01:11:17Z (GMT). No. of bitstreams: 3 REBAND-THESIS-2021.pdf: 551747 bytes, checksum: e615e84f6c92ac5d84c38344f943bd41 (MD5) Reband_Thesis_04232021.zip: 576023 bytes, checksum: f2fafb733fd3185741bf2ebce9d7736b (MD5) LICENSE.txt: 4208 bytes, checksum: 561ec01cc3db715782895610b58d39fa (MD5) Previous issue date: 2021-04-27"],"dc:format":["application/pdf"],"dc:identifier":["http://hdl.handle.net/2142/110568"],"dc:language":["en"],"dc:rights":["©2021 John Reband"],"dc:subject":["Electric Aircraft","Powertrain","Conceptual Design","Aircraft Conceptual Design"],"dc:title":["Power system sizing and analysis for electric aircraft conceptual design"],"dc:type":["text","Thesis"],"thesis:degree_discipline":["Electrical & Computer Engr"],"thesis:degree_level":["Thesis"],"thesis:degree_name":["M.S."],"thesis:institution_name":["University of Illinois at Urbana-Champaign"]},"updated_at":"2026-07-22T22:24:52Z"}