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Mostrati risultati da 1 a 20 di 20
Tipologia Anno Titolo Titolo inglese Autore File
Lauree magistrali 2021 ANALISI NUMERICA DELLA FISICA DELLA PROPULSIONE A RAZZO IBRIDA NUMERICAL ANALYSIS OF HYBRID ROCKET COMBUSTION PHYSICS RAMPAZZO, ALESSANDRO
Lauree magistrali 2020 Bi-dimensional heat exchange model of a regenerative cooled nozzle for hydrogen peroxyde bi-propellant thrusters Bi-dimensional heat exchange model of a regenerative cooled nozzle for hydrogen peroxyde bi-propellant thrusters CANTIANI, RICCARDO
Lauree magistrali 2023 Design of a 10 N HTP-Propane liquid bipropellant thruster for a reusable spacecraft Design of a 10 N HTP-Propane liquid bipropellant thruster for a reusable spacecraft QUINZI, GIULIA
Lauree magistrali 2021 Design of an advanced microturbine generator for light electric aircrafts Design of an advanced microturbine generator for light electric aircrafts DE ROSSI, FEDERICO
Lauree magistrali 2022 Design of the nose cone of a transonic sounding rocket Design of the nose cone of a transonic sounding rocket DAPIT, GIOVANNI
Lauree magistrali 2022 Electric Pump Cooling System Design For High Performance Moon Engine Electric Pump Cooling System Design For High Performance Moon Engine CANDELATO, MATTIA
Lauree magistrali 2021 Fluid dynamic analysis and development of a 1 N bipropellant liquid rocket combustion chamber - Zheng, Matteo
Lauree magistrali 2022 Investigation of different strategies for access to space and positioning of small satellites Investigation of different strategies for access to space and positioning of small satellites FIORIO, MATTEO
Lauree magistrali 2022 Mass flow modulation with a variable area cavitating Venturi flow control valve Mass flow modulation with a variable area cavitating Venturi flow control valve ROMANI, EDOARDO
Lauree triennali 2022 Metodi di protezione termica e raffreddamento degli ugelli dei motori a razzo Thrust chamber thermal protection and cooling methods for rocket engines MASSIMO, ALESSANDRO
Lauree magistrali 2022 Numerical modeling of flame acceleration and transition to detonation in narrow channels Numerical modeling of flame acceleration and transition to detonation in narrow channels NUTI, LEONARDO
Lauree magistrali 2023 Ottimizzazione di una microturbina con recuperatore e intercooler per aerei ibridi Optimization of an intercooled-­recuperated microturbine for hybrid aircraft RINALDI, JESSICA
Lauree magistrali 2021 PRELIMINARY DESIGN OF A NITROMETHANE MEMS THRUSTER PRELIMINARY DESIGN OF A NITROMETHANE MEMS THRUSTER VENTURINI, STEFANO
Lauree magistrali 2020 Preliminary design of a nitromethane rocket engine Preliminary design of a nitromethane rocket engine BERTO, FEDERICO
Lauree triennali 2022 Progettazione e dimensionamento delle alette del razzo SFR I nell'ambito del progetto universitario Thrust Design and sizing of the SFR I rocket fins as part of the Thrust university project SPILLER, DAVIDE
Lauree magistrali 2020 Progetto e realizzazione del sistema di recupero di un sounding rocket ibrido - Trabuio, Alessio
Lauree magistrali 2020 Safety Range and Load Analyses of a Hybrid Sounding Rocket - Zeni, Lucia
Lauree magistrali 2021 STUDIO FLUIDODINAMICO DI UNA POMPA A EMISSIONE PARZIALE PER MOTORI A RAZZO IBRIDI FLUID DYNAMIC STUDY OF A PARTIAL EMISSION PUMP FOR HYBRID ROCKET MOTORS BERTOSIN, PAOLO
Lauree magistrali 2022 Studio preliminare di un dirigibile con motore a turbina innovativo a zero emissioni utilizzante Tridyne Preliminary study of an airship with an innovative zero emission Tridyne turbine PANNO, SALVATORE
Lauree magistrali 2022 Valutazione preliminare delle configurazioni delle turbomacchine per un generatore elettrico a microturbina con intercooler e recuperatore Preliminary assessment of turbomachinery configurations for an intercooled-recuperated microturbine electric generator LANA, GIULIA
Mostrati risultati da 1 a 20 di 20
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