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Thermal analysis for the Teidesat/Alisio Cubesats
| dc.contributor.advisor | Martín Mateos, Isabel Teresa | es_ES |
| dc.contributor.advisor | González De Chaves, Pablo | es_ES |
| dc.contributor.author | González Vilar, Javier | es_ES |
| dc.contributor.other | Grado En Ingeniería Mecánica | es_ES |
| dc.date.accessioned | 2019-06-25T08:25:20Z | |
| dc.date.available | 2019-06-25T08:25:20Z | |
| dc.date.issued | 2019 | es_ES |
| dc.identifier.uri | http://riull.ull.es/xmlui/handle/915/14517 | |
| dc.description.abstract | The aim of this project is to analyse the temperature that a 1U CubeSat will encounter on orbit, and consequently produce a first approach to the thermal design of the satellite Teidesat. The Microsatellite project team from IACTEC is also petitionary of this bachelor thesis because they are interested in performing thermal analysis in a CubeSat, so that they can develop their own nanosatellites. IACTec Microsatellites team is developing the Payload for a 3U CubeSat mission called ALISIO I, this case will be analysed too. | en |
| dc.format.mimetype | application/pdf | es_ES |
| dc.language.iso | es | es_ES |
| dc.rights | Licencia Creative Commons (Reconocimiento-No comercial-Sin obras derivadas 4.0 Internacional) | es_ES |
| dc.rights.uri | https://creativecommons.org/licenses/by-nc-nd/4.0/deed.es_ES | es_ES |
| dc.subject | Satelite | es_ES |
| dc.subject | Instituto Astrofísico de Canarias | es_ES |
| dc.subject | Teidesat | es_ES |
| dc.title | Thermal analysis for the Teidesat/Alisio Cubesats | es_ES |
| dc.type | info:eu-repo/semantics/bachelorThesis | |
| dc.subject.keyword | Instituto Astrofísico de Canarias | |
| dc.subject.keyword | Satélite | |
| dc.subject.keyword | Teidesat |
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