Sfoglia per Relatore
Measurement of powder ignition temperatures under fast heating rates through optical pyrometry
2017/2018 GINELLI, CHIARA MARIA
Mechanical activation of Al-Mg fuel powders for green propellants
2014/2015 ARDALIC, JOVAN
Mechanically activated powders as alternative to nanometric aluminum in solid propellants : potentialities and perspectives
2017/2018 CICCIARELLI, CLARISSA
Methods for optimizing a Monte Carlo campaign: sampling and representativeness considerations on an aerospace model
2023/2024 Larocca, Rocco
Miscele di micro-alluminio e PTFE : caratterizzazione ed effetti di processi di attivazione meccanica
2013/2014 GIANNONE, CORRADO
Mission analysis of a Mars ascent vehicle based on nuclear thermal propulsion
2022/2023 GUNASEKAR, SOORAJ
Modeling and on-ground testing of self-pressurized liquid propellant behavior for in-orbit refueling
2020/2021 Foletti, Nicola
Modeling of a HRM canister-launched missile using OpenModelica
2017/2018 MARCHESAN, DAVIDE
Modelling of a Controlled Re-entry of VTVL Vehicle
2021/2022 RESTUCCIA, MASSIMILIANO
Modelling Thermite-aided Spacecraft Demise during Re-entry
2021/2022 Brindavanam, Dinesh
Monte Carlo method for uncertainty quantification of SRM internal ballistic model
2013/2014 VIGANÒ, DAVIDE
A new numerical model to represent two-phase injection flows
2021/2022 Parducci, Alessandro
Non-reacting multiphase flow inside a 2D rocket motor chamber
2019/2020 OTTINÀ, VINCENZO
Nuclear electric propulsion in the future of space exploration
2022/2023 MAZZA, GIULIANO
Numerical investigation and propulsive performance evaluation of pulse detonation thruster
2022/2023 SOMMA, UMBERTO
Numerical simulation of gas-particle two-phase flow in a nozzle with ANSYS Fluent
2021/2022 PASTURENZI, LORENZO
Numerical simulation of nitrous oxide catalytic decomposition
2016/2017 LOCATELLI, MATTEO
Optimization study for the production of the P120
2021/2022 TAUPIN, HORTENSE ANDREA MADELEINE
Oxidizer lean solid propellants for air augmented rocket propulsion
2014/2015 COLCIAGO, SIMONE
Physical modeling of rocket engine components in the European space propulsion system simulation environment for Airbus Safran launchers use
2015/2016 VOLPI, GIULIA
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