Sfoglia per Relatore
Conceptual design for assembly method in aerospace : how to conceive optimized product architectures oriented to manufacturing and assembly
2017/2018 FORMENTINI, GIOVANNI
Conceptual design of a water electrolysis propulsion system for a 3U CubeSat
2021/2022 Paletta, Daniele
Conceptual design, system and performance analysis of a water electrolysis propulsion system for CubeSats
2022/2023 Paldino, Gian Marco
Design and simulation of a 1N hydrogen peroxide monopropellant thruster
2018/2019 URAS, ANDREA
Design di un ugello di tipo Aerospike e della linea sperimentale per la sua validazione
2013/2014 MONALDI, ANDREA
Design of a green-propellant based micro-thruster
2020/2021 Sharma, Shreya
Design of a paraffin-hydrogen peroxide hybrid rocket
2019/2020 SOARDI, ELENA
Design, optimization and sizing of a Water Electrolysis Propulsion (WEP) system for CubeSats
2021/2022 Chivukula, Varun
Design, realizzazione e test di un endoreattore ibrido di tipo vortex flow pancake
2014/2015 MESSINA, MICHELE
Development and Analysis of Water Electrolysis Propulsion Systems for Cubesats and Small Satellites.
2023/2024 BHEMESETTI, SWATHI LEKHA
Development and validation of a DSMC method for industrial application
2014/2015 GENTILHOMME, JULIEN
Development of a hydrogen peroxide monopropellant micro-thruster
2018/2019 OLCUCUOGLU, BERKE
Diagnostic methodologies in a blow-down hypersonic tunnel for rocket based combined cycle engine performance characterization
2017/2018 DAVIS, SNEHA
Droplet entrainment modeling for paraffin-based fuels in hybrid rocket engines
2014/2015 VENEZIANI, LUCA
Effetti di geometria del grano combustibile nei processi di combustione in motori ibridi per la propulsione spaziale
2010/2011 PADOVESE, MATTEO
Entrainment effects on combustion processes in paraffin-based hybrid rocket motors
MILOVA, PRASKOVIA
Entrainment phenomena of paraffin based fuels in hybrid rocket engines combustion
2011/2012 LOSCERTALES CASTANOS, FRANCISCO JAVIER
Entrainment phenomenon in liquefying solid fuels combustion
2018/2019 MAZZALI, SARA
Environmentally friendly design of Spacex Falcon Heavy with LH2-LOX core and ADN-GAP boosters
2016/2017 PELLEGRINO, DANIELE
Eulerian multi-fluid method for aeronautical spray combustion
2019/2020 ZACCARIA, FILIPPO
Legenda icone accesso al fulltext
- File accessibili da tutti
- File accessibili dagli utenti autorizzati
- File accessibili da tutti o solo dagli utenti autorizzati, a partire dalla la data indicata nella scheda
- File non accessibili