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dc.contributorCarreras Planells, Ramón
dc.contributor.authorFerrer González, Carlos
dc.date.accessioned2010-12-16T15:24:29Z
dc.date.available2010-12-16T15:24:29Z
dc.date.issued2010-09
dc.identifier.urihttp://hdl.handle.net/2099.1/10552
dc.description.abstractAccording to the concept of a fluid-bipropellant rocket engine proposed in Design of a rocket engine fed with oxygen and methane in gaseous phase for educational purposes [TR01], a preliminary test stand design for the prediction and validation of the main performances of this engine has been developed. The main sensors and transducers are selected to measure the stated performances. After the proposed instrumentation, a virtual panel control has been also carried out.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus::Coets
dc.subjectÀrees temàtiques de la UPC::Enginyeria mecànica::Motors::Motors de combustió interna
dc.subject.lcshRocket engines
dc.subject.lcshLiquid propellant rocket engines
dc.titleStudy of a static rocket test stand system for setting the performances of a rocket engine fed with oxygen and methane in gaseous phase
dc.typeMaster thesis (pre-Bologna period)
dc.subject.lemacCoets (Aeronàutica) -- Motors
dc.subject.lemacMotors de combustió interna
dc.rights.accessOpen Access
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola Tècnica Superior d'Enginyeries Industrial i Aeronàutica de Terrassa


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Except where otherwise noted, content on this work is licensed under a Creative Commons license: Attribution-NonCommercial-NoDerivs 3.0 Spain