Design and construction of an upgraded hybrid rocket

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dc.contributor.advisor Merino Martínez, Mario
dc.contributor.author Esteban Corchado, Sara
dc.date.accessioned 2017-02-16T12:46:46Z
dc.date.available 2017-02-16T12:46:46Z
dc.date.issued 2016-02
dc.date.submitted 2016-03-09
dc.identifier.uri http://hdl.handle.net/10016/24213
dc.description.abstract Hybrid rockets are a type of chemical space propulsion that is nowadays still in an experimental phase, but that can become one of the most important propulsion technologies due to its advantages with respect to the existing ones. The present work consist on developing an upgraded hybrid rocket model which has been modified with respect to the existing one in order to obtain better performances and results. The aim of this project is to create a safer model with a safer ignition system as well as a fully redesigned gas-injection and thrust measurement system. Also, a mathematical one-dimensional model has been implemented in order to predict and study the behavior of the hybrid rocket model to achieve a better comprehension of this topic. The ultimate purpose of the project is to acquire a deep understanding concerning the space propulsion, concretely the one associated with hybrid rocket propulsion.
dc.format.mimetype application/pdf
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 Hybrid rockets
dc.subject.other Propulsion technologies
dc.subject.other Mathematical models
dc.title Design and construction of an upgraded hybrid rocket
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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