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Test Equipment Design for a Space System
dc.contributor.advisor | Roldán Aranda, Andrés María | |
dc.contributor.author | Romero García, Miguel | |
dc.contributor.other | GranaSAT - Grupo de Electronica Aeroespacial | es_ES |
dc.date.accessioned | 2022-04-22T10:20:52Z | |
dc.date.available | 2022-04-22T10:20:52Z | |
dc.date.issued | 2021 | |
dc.identifier.uri | http://hdl.handle.net/10481/74461 | |
dc.description.abstract | The aim of this project is to show the work carried out by the author during his work experience at the company Tecnobit-Grupo Oesia, where he has been in charge of the design of the test equipment that will be responsible for verifying the operability of the distribution electronics developed at the company for the SPAINSAT NG I and SPAINSAT NG II satellites. During the development of this document, we will start by explaining how a space system is developed, followed by the requirements agreed with the different companies involved in the project, and later, with the design of the EGSE developed at the company by the author. Once finished, the implementation process will be shown, as well as the budget that accompanies this part of the project. | es_ES |
dc.language.iso | spa | es_ES |
dc.rights | Atribución-NoComercial-SinDerivadas 3.0 España | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/es/ | * |
dc.subject | Electrical Ground Support Equipment | es_ES |
dc.subject | PCB Design | es_ES |
dc.subject | European Cooperation for Space Standardization | es_ES |
dc.subject | SolidWorks | es_ES |
dc.subject | RFCB | es_ES |
dc.subject | MCCM | es_ES |
dc.subject | DL | es_ES |
dc.title | Test Equipment Design for a Space System | es_ES |
dc.type | bachelor thesis | es_ES |
dc.rights.accessRights | open access | es_ES |
dc.type.hasVersion | VoR | es_ES |