{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/101623"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/101623","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Design of a scalable nano university satellite bus (IlliniSat-2 bus) command and data handling system and power system","abstract":"IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The IlliniSat-2 is required to be capable of operating a nanosatellite from size 1.5U (10x10x17cm) to 6U (10x22.6x36.6cm) and carrying up to three science payloads. The challenge with IlliniSat-2 bus is the requirement for the wide-range scalability. The major contribution of this work includes the requirements, design, testing, and validation of two parts of the IlliniSat-2 bus systems: Command and Data Handling system and Power Generation and Distribution system. This work also contributes the lessons learned throughout the implementation of the flight hardware. So far, five missions are using IlliniSat-2 bus to carry their science payloads: LAICE, CubeSail, SpaceICE, SASSI^2 and CAPSat. CubeSail satellite was fully constructed and delivery to the launcher on April 12th, 2018. The tentative launch date as of this publication is August 31st, 2018. SpaceICE, SASSI^2 and CAPSat are three missions developed as parts of the NASA Science Mission Directorate’s (SMD) Undergraduate Student Instrument Program (USIP). Those three satellites are being constructed as of this publication and will be delivered to perspective launchers by the end of August. LAICE satellite was constructed and is awaiting to be delivered to the launch in November 1st, 2018.","abstract_html":"IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The IlliniSat-2 is required to be capable of operating a nanosatellite from size 1.5U (10x10x17cm) to 6U (10x22.6x36.6cm) and carrying up to three science payloads. The challenge with IlliniSat-2 bus is the requirement for the wide-range scalability. The major contribution of this work includes the requirements, design, testing, and validation of two parts of the IlliniSat-2 bus systems: Command and Data Handling system and Power Generation and Distribution system. This work also contributes the lessons learned throughout the implementation of the flight hardware. So far, five missions are using IlliniSat-2 bus to carry their science payloads: LAICE, CubeSail, SpaceICE, SASSI^2 and CAPSat. CubeSail satellite was fully constructed and delivery to the launcher on April 12th, 2018. The tentative launch date as of this publication is August 31st, 2018. SpaceICE, SASSI^2 and CAPSat are three missions developed as parts of the NASA Science Mission Directorate’s (SMD) Undergraduate Student Instrument Program (USIP). Those three satellites are being constructed as of this publication and will be delivered to perspective launchers by the end of August. LAICE satellite was constructed and is awaiting to be delivered to the launch in November 1st, 2018.","abstract_has_math":false,"creators":["Wang, Zipeng"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Ghosh, Alexander R. M.","Swenson, Gary R."],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2018,"date_issued":"2018-09-27T16:18:02Z","date_published":"2018-09-27T16:18:02Z","updated_at":"2026-07-22T22:24:40Z","subjects":["CubeSat","Nano-satellite","IlliniSat-2","C&DH","Spacecraft Power Generation and Delivery:"],"languages":["en"],"rights":["Copyright 2018 Zipeng Wang"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"http://hdl.handle.net/2142/101623","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Ghosh, Alexander R. M.","Swenson, Gary R."]},{"key":"dc:creator","label":"Author","values":["Wang, Zipeng"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2018-09-27T16:18:02Z","2018-07-19","2018-08"]},{"key":"dc:type","label":"Dc Type","values":["text"]},{"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":["CubeSat","Nano-satellite","IlliniSat-2","C&DH","Spacecraft Power Generation and Delivery:"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en"]},{"key":"dc:rights","label":"Dc Rights","values":["Copyright 2018 Zipeng Wang"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["http://hdl.handle.net/2142/101623"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The IlliniSat-2 is required to be capable of operating a nanosatellite from size 1.5U (10x10x17cm) to 6U (10x22.6x36.6cm) and carrying up to three science payloads. The challenge with IlliniSat-2 bus is the requirement for the wide-range scalability. The major contribution of this work includes the requirements, design, testing, and validation of two parts of the IlliniSat-2 bus systems: Command and Data Handling system and Power Generation and Distribution system. This work also contributes the lessons learned throughout the implementation of the flight hardware. So far, five missions are using IlliniSat-2 bus to carry their science payloads: LAICE, CubeSail, SpaceICE, SASSI^2 and CAPSat. CubeSail satellite was fully constructed and delivery to the launcher on April 12th, 2018. The tentative launch date as of this publication is August 31st, 2018. SpaceICE, SASSI^2 and CAPSat are three missions developed as parts of the NASA Science Mission Directorate’s (SMD) Undergraduate Student Instrument Program (USIP). Those three satellites are being constructed as of this publication and will be delivered to perspective launchers by the end of August. LAICE satellite was constructed and is awaiting to be delivered to the launch in November 1st, 2018.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2018-09-27 without embargo terms","The student, Zipeng Wang, accepted the attached license on 2018-07-19 at 10:17.","The student, Zipeng Wang, submitted this Thesis for approval on 2018-07-19 at 10:35.","This Thesis was approved for publication on 2018-07-19 at 10:59.","DSpace SAF Submission Ingestion Package generated from Vireo submission #12936 on 2018-09-27 at 10:49:54","Made available in DSpace on 2018-09-27T16:18:02Z (GMT). No. of bitstreams: 3 WANG-THESIS-2018.pdf: 6427322 bytes, checksum: 06f0b120dc1b46fedc57d4ee921c0292 (MD5) Thesis Souce Files.zip: 118947893 bytes, checksum: 2bb2837920357fdf1aa8cda634ba54f3 (MD5) LICENSE.txt: 4208 bytes, checksum: c76b97ae679f542c9890d1a8b9ccc0ab (MD5) Previous issue date: 2018-07-19"]},{"key":"dc:format","label":"Dc Format","values":["application/pdf"]},{"key":"dc:title","label":"Title","values":["Design of a scalable nano university satellite bus (IlliniSat-2 bus) command and data handling system and power system"]}]}],"canonical_facts":{"dc:contributor":["Ghosh, Alexander R. M.","Swenson, Gary R."],"dc:creator":["Wang, Zipeng"],"dc:date":["2018-09-27T16:18:02Z","2018-07-19","2018-08"],"dc:description":["IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The IlliniSat-2 is required to be capable of operating a nanosatellite from size 1.5U (10x10x17cm) to 6U (10x22.6x36.6cm) and carrying up to three science payloads. The challenge with IlliniSat-2 bus is the requirement for the wide-range scalability. The major contribution of this work includes the requirements, design, testing, and validation of two parts of the IlliniSat-2 bus systems: Command and Data Handling system and Power Generation and Distribution system. This work also contributes the lessons learned throughout the implementation of the flight hardware. So far, five missions are using IlliniSat-2 bus to carry their science payloads: LAICE, CubeSail, SpaceICE, SASSI^2 and CAPSat. CubeSail satellite was fully constructed and delivery to the launcher on April 12th, 2018. The tentative launch date as of this publication is August 31st, 2018. SpaceICE, SASSI^2 and CAPSat are three missions developed as parts of the NASA Science Mission Directorate’s (SMD) Undergraduate Student Instrument Program (USIP). Those three satellites are being constructed as of this publication and will be delivered to perspective launchers by the end of August. LAICE satellite was constructed and is awaiting to be delivered to the launch in November 1st, 2018.","Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2018-09-27 without embargo terms","The student, Zipeng Wang, accepted the attached license on 2018-07-19 at 10:17.","The student, Zipeng Wang, submitted this Thesis for approval on 2018-07-19 at 10:35.","This Thesis was approved for publication on 2018-07-19 at 10:59.","DSpace SAF Submission Ingestion Package generated from Vireo submission #12936 on 2018-09-27 at 10:49:54","Made available in DSpace on 2018-09-27T16:18:02Z (GMT). No. of bitstreams: 3 WANG-THESIS-2018.pdf: 6427322 bytes, checksum: 06f0b120dc1b46fedc57d4ee921c0292 (MD5) Thesis Souce Files.zip: 118947893 bytes, checksum: 2bb2837920357fdf1aa8cda634ba54f3 (MD5) LICENSE.txt: 4208 bytes, checksum: c76b97ae679f542c9890d1a8b9ccc0ab (MD5) Previous issue date: 2018-07-19"],"dc:format":["application/pdf"],"dc:identifier":["http://hdl.handle.net/2142/101623"],"dc:language":["en"],"dc:rights":["Copyright 2018 Zipeng Wang"],"dc:subject":["CubeSat","Nano-satellite","IlliniSat-2","C&DH","Spacecraft Power Generation and Delivery:"],"dc:title":["Design of a scalable nano university satellite bus (IlliniSat-2 bus) command and data handling system and power system"],"dc:type":["text"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis"],"thesis:degree_name":["M.S."],"thesis:institution_name":["University of Illinois at Urbana-Champaign"]},"updated_at":"2026-07-22T22:24:40Z"}