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dc.contributorPérez Mansilla, Sonia
dc.contributor.authorDe la Torre González, Alex
dc.description.abstractThis study is addressed to design and build a nozzle for a first stage of a solid propellant APCP (Ammonium Perchlorate Composite Propellant) based as a part of an EETAC university grant. We will use the simulator Moon2.0 to design the basics nozzle parameters. A series of material tests should be done in order to validate the technology based on composite materials such as Carbon FOAM, graphite and ceramics. In this final bachelor work, we try to check if this design is useful for a project like the low cost Wiki-Launcher less than 100 kg mass that puts in LEO (Low Earth Orbit) orbit a femtosatellite of less than 100 gram mass.
dc.publisherUniversitat Politècnica de Catalunya
dc.rightsAttribution-NonCommercial-ShareAlike 3.0 Spain
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus::Coets
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Astronàutica
dc.subject.lcshArtificial satellites
dc.subject.lcshRockets (Aeronautics)
dc.subject.otherLow cost rocket
dc.titleDesign and implementation of a first stage nozzle for a low cost mini-launcher
dc.typeBachelor thesis
dc.subject.lemacSatèl·lits artificials
dc.subject.lemacCoets (Aeronàutica)
dc.rights.accessOpen Access
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola d'Enginyeria de Telecomunicació i Aeroespacial de Castelldefels

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Attribution-NonCommercial-ShareAlike 3.0 Spain
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