The thesis aims at developing a numerical code to study the electromagnetic wave-plasma interaction phenomena critical for the operation of electrodeless thrusters, particularly, the Electron Cyclotron Resonance (ECR) Thruster under development in the European H2020 MINOTOR project. Current in-space Electric Propulsion technologies are presented with special attention to their advantageous characteristics compared to conventional techniques. Among those, electrodeless thrusters emerge as efficient and durable alternatives for future propulsion systems. The main limitation hindering the implementation of these devices is the complicated physical phenomena governing the fundamental operational stages i.e. the plasma heating and ionizat...
An axisymmetric fluid model for weakly-collisional, magnetized electrons is introduced and coupled ...
The focus of this research program is experimentally characterizing and developing advanced plasma p...
The optimization of the efficiency of an ECR-based charge breeder is a twofold task: efforts must be...
Proceeding of: 35th International Electric Propulsion Conference (IEPC), October 8-12, 2017, Atlanta...
Proceeding of: Space Propulsion Conference, SP 2018,14-18 mayo, SevillaThis paper presents the devel...
Special Issue on Space Plasma PropulsionAn axisymmetric, finite difference frequency domain model is...
This Thesis presents an investigation of the plasma-wave interaction in Helicon Plasma Thrusters (H...
A two-dimensional, full-wave, frequency domain, cold plasma model is used to study electromagnetic ...
This paper has been presented at the 36th International Electric Propulsion ConferenceWe present the...
An electron-cyclotron resonance thruster (ECRT) prototype is simulated numerically, using two couple...
International audienceA coaxial ECR thruster is simulated using a 1D3V electromagnetic Particle-In-C...
An axisymmetric fluid model for weakly-collisional, magnetized electrons is introduced and coupled ...
The focus of this research program is experimentally characterizing and developing advanced plasma p...
The optimization of the efficiency of an ECR-based charge breeder is a twofold task: efforts must be...
Proceeding of: 35th International Electric Propulsion Conference (IEPC), October 8-12, 2017, Atlanta...
Proceeding of: Space Propulsion Conference, SP 2018,14-18 mayo, SevillaThis paper presents the devel...
Special Issue on Space Plasma PropulsionAn axisymmetric, finite difference frequency domain model is...
This Thesis presents an investigation of the plasma-wave interaction in Helicon Plasma Thrusters (H...
A two-dimensional, full-wave, frequency domain, cold plasma model is used to study electromagnetic ...
This paper has been presented at the 36th International Electric Propulsion ConferenceWe present the...
An electron-cyclotron resonance thruster (ECRT) prototype is simulated numerically, using two couple...
International audienceA coaxial ECR thruster is simulated using a 1D3V electromagnetic Particle-In-C...
An axisymmetric fluid model for weakly-collisional, magnetized electrons is introduced and coupled ...
The focus of this research program is experimentally characterizing and developing advanced plasma p...
The optimization of the efficiency of an ECR-based charge breeder is a twofold task: efforts must be...