Sfoglia per Relatore
A non-conventional hybrid rocket motor for de-orbiting applications
2016/2017 MARINO, FRANCESCO
Aluminium composites for regression rate enhancement in solid fuels for hybrid rocket propulsion
2014/2015 MYZYRI, JUXHIN
Ambre - the first prototype of a hybrid autophage space launcher
2022/2023 Mazzella, Vincenzo
Analysis of quasi-steady and forced transient burning of paraffin-based fuels
2019/2020 Minini, Michele
An analysis of the methods for the enhancement of mechanical properties of paraffin-based fuels
2019/2020 Cirina, Andrea
Ballistics of liquefying fuel formulations : time-resolved techniques for regression rate determination
2019/2020 Chiappa, Sebastiano
Burning behaviour investigation of a lab-scale vortex combustion hybrid rocket motor
2017/2018 LISI, FRANCESCO
Burning of liquefying paraffin-based fuels in a vortex flow hybrid rocket engine with non-conventional configuration
2020/2021 Visinoni, Julian
Burning tests of a vortex flow hybrid rocket engine for post-mission disposal
2017/2018 LAO AMORES, ESPERANZA MARIA
Capacitance sensor: numerical and experimental applications in the aerospace field
2023/2024 Paoletti, Luca Giorgio
Cellular structures as reinforcing strategy in paraffin-based fuels for HRE: oxidizer, injection and grain scale-up effects
2022/2023 Garcidueñas Correa, Alam Uziel
A CFD Analysis on HREs Using Swirl Injection and Paraffin-based Fuel
2022/2023 Paterniti, Andrea
Characterization of nanometer-sized aluminium dispersion in polymeric matrixes
2015/2016 NAPOLI, ALBERTO
Coated aluminum powders for innovative hybrid rocket fuel formulations
2015/2016 PIANELLI, MICHELE
Combined methods for paraffin-based fuel reinforcement : armored grain and blending with polymers
2019/2020 Tahar, Samy
Combustion chamber height effect on VFP engine
2016/2017 De MARCO, STEFANO
Comprehensive film cooling modeling: from liquid to gaseous coolant layer for thrust chamber thermal protection
2023/2024 Rondena, Giulia
Design and test of a vortex flow hybrid rocket motor
2014/2015 CARLOTTI, STEFANIA
Design of a hybrid rocket engine with thrust levels from 400 N to 1 kN
2018/2019 GIUSTO, PIETRO
Design of a test bench for firing tests of a lab-scale hybrid rocket engine
2016/2017 DI CICCO, MARIO ALBERTO
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