Studente Rostello, Marco
Facoltà/Dipartimento Scuola di Ingegneria
Corso di studio INGEGNERIA AEROSPAZIALE
Anno Accademico 2017-10-13
Titolo originale Preliminar sizing of an electrospray thruster
Abstract As there isn’t a precise model of electrospray thrusters what I will try to do in this master thesis is to find a mathematical model that describes them in a simple way. After exposing some physical concepts I will study the physics of conductive liquids and then study the dynamics of the fluid during the operation with the purpose of calculating the propulsive parameters. In the end all equations found will be grouped together to implement a Matlab code setting with many initial conditions
Parola chiave electric propulsion, electrospray
Relatore Pavarin, Daniele
Correlatore Benavides, Efrén Moreno
Appare nelle tipologie: Lauree magistrali
File in questo prodotto:
File Dimensione Formato  
Rostello_Marco_1109399.pdf 1.38 MB Adobe PDF Visualizza/Apri

The text of this website © Università degli studi di Padova. Full Text are published under a non-exclusive license. Metadata are under a CC0 License

Utilizza questo identificativo per citare o creare un link a questo documento: http://hdl.handle.net/20.500.12608/28517