2026-04-13T01:52:41Zhttps://recercat.cat/oai/request

oai:recercat.cat:2099.1/105522025-07-17T16:32:03Zcom_2072_1033col_2072_452951

Study of a static rocket test stand system for setting the performances of a rocket engine fed with oxygen and methane in gaseous phase Ferrer González, Carlos Carreras Planells, Ramón Àrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus::Coets Àrees temàtiques de la UPC::Enginyeria mecànica::Motors::Motors de combustió interna Rocket engines Liquid propellant rocket engines Coets (Aeronàutica) -- Motors Motors de combustió interna 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. 2010-09 Master thesis (pre-Bologna period) https://hdl.handle.net/2099.1/10552 eng http://creativecommons.org/licenses/by-nc-nd/3.0/es/ Open Access Attribution-NonCommercial-NoDerivs 3.0 Spain application/pdf Universitat Politècnica de Catalunya