dc.contributor
Carreras Planells, Ramón
dc.contributor.author
Ferrer González, Carlos
dc.identifier
https://hdl.handle.net/2099.1/10552
dc.description.abstract
According 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.format
application/pdf
dc.publisher
Universitat Politècnica de Catalunya
dc.rights
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.rights
Attribution-NonCommercial-NoDerivs 3.0 Spain
dc.subject
Àrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus::Coets
dc.subject
Àrees temàtiques de la UPC::Enginyeria mecànica::Motors::Motors de combustió interna
dc.subject
Rocket engines
dc.subject
Liquid propellant rocket engines
dc.subject
Coets (Aeronàutica) -- Motors
dc.subject
Motors de combustió interna
dc.title
Study of a static rocket test stand system for setting the performances of a rocket engine fed with oxygen and methane in gaseous phase
dc.type
Master thesis (pre-Bologna period)
