Design and analysis of μPPT

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dc.contributor.advisor Merino Martínez, Mario
dc.contributor.author Rubio García, Adrián
dc.date.accessioned 2019-12-03T11:27:38Z
dc.date.available 2019-12-03T11:27:38Z
dc.date.issued 2018-10
dc.date.submitted 2018-10-18
dc.identifier.uri http://hdl.handle.net/10016/29283
dc.description.abstract Cubesats constitute an inexpensive access to space and are one of the fastest growing technologies in the space industry. A micro pulsed plasma thruster (μPPT) is going to be modeled and designed in this paper to accomplish the requirements implied in cubesat dimensions and to perform drag compensation for an specific satellite mission. The performance of the thruster is going to be analyzed to fulfill, in the most effective way, the mission requirements.
dc.language.iso eng
dc.rights Atribución-NoComercial-SinDerivadas 3.0 España
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject.other Cubesats
dc.subject.other Space industry
dc.subject.other Micro Pulsed Plasma Thruster (μPPT)
dc.subject.other Satellites
dc.subject.other Space mission
dc.title Design and analysis of μPPT
dc.type bachelorThesis
dc.subject.eciencia Aeronáutica
dc.rights.accessRights openAccess
dc.description.degree Ingeniería Aeroespacial
dc.contributor.departamento Universidad Carlos III de Madrid. Departamento de Bioingeniería e Ingeniería Aeroespacial
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