Study of a thrust vectoring system for rockets through a pressurized air test bench
| dc.contributor | González Díez, David |
| dc.contributor | Solé Busquet, Jaume |
| dc.contributor.author | Tió Malo, Xavier |
| dc.contributor.other | Universitat Politècnica de Catalunya. Departament d'Enginyeria Electrònica |
| dc.date.accessioned | 2020-05-04T12:14:20Z |
| dc.date.issued | 2017-06-10 |
| dc.identifier.uri | http://hdl.handle.net/2117/186163 |
| dc.description.abstract | Aiming to be the first step towards the design of a fully operational stabilization system for rockets, thebuilding of a model is done representing the attitudeof a rocket with anactive stability system. Several tests are done with the model both static and dynamic with different type of sensors that give us a view of the response of the system to different situations. Finally, it is described how the model could be upgradedand which steps follow to get a reliable stabilization system. |
| dc.language.iso | eng |
| dc.publisher | Universitat Politècnica de Catalunya |
| dc.subject | Àrees temàtiques de la UPC::Enginyeria electrònica |
| dc.subject.lcsh | Rocket engines |
| dc.title | Study of a thrust vectoring system for rockets through a pressurized air test bench |
| dc.type | Bachelor thesis |
| dc.subject.lemac | Coets (Aeronàutica) -- Motors |
| dc.identifier.slug | 205-1107 |
| dc.rights.access | Restricted access - author's decision |
| dc.date.lift | 10000-01-01 |
| dc.date.updated | 2019-10-24T12:27:36Z |
| dc.audience.educationlevel | Grau |
| dc.audience.mediator | Escola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa |
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