Coupled plasma transport and electromagnetic wave simulation of an ECR thruster
An electron-cyclotron resonance thruster (ECRT) prototype is simulated numerically, using
two coupled models: a hybrid particle-in-cell/fluid model for the integration of the plasma …
two coupled models: a hybrid particle-in-cell/fluid model for the integration of the plasma …
Using electron fluid models to analyze plasma thruster discharges
E Ahedo - Journal of Electric Propulsion, 2023 - Springer
Fluid models of the slow-dynamics of magnetized, weakly-collisional electrons lead to build
computationally-affordable, long-time simulations of plasma discharges in Hall-effect and …
computationally-affordable, long-time simulations of plasma discharges in Hall-effect and …
Development of a lumping methodology for the analysis of the excited states in plasma discharges operated with argon, neon, krypton, and xenon
N Souhair, M Magarotto, E Majorana, F Ponti… - Physics of …, 2021 - pubs.aip.org
In this paper, a methodology is presented to compute the plasma properties (eg,, density
and temperature) accounting for the dynamics of the excited states. The proposed strategy …
and temperature) accounting for the dynamics of the excited states. The proposed strategy …
[HTML][HTML] Hybrid plasma simulations of a magnetically shielded Hall thruster
J Perales-Díaz, A Domínguez-Vázquez… - Journal of Applied …, 2022 - pubs.aip.org
Numerical simulations of a magnetically shielded Hall effect thruster with a centrally
mounted cathode are performed with an axisymmetric hybrid particle-in-cell/fluid code and …
mounted cathode are performed with an axisymmetric hybrid particle-in-cell/fluid code and …
Analysis of a cusped helicon plasma thruster discharge
Experiments and simulations are used to analyze a compact helicon plasma thruster with a
cusp in its internal magnetic field. The former rely on a compensated Langmuir probe and a …
cusp in its internal magnetic field. The former rely on a compensated Langmuir probe and a …
Numerical model of a helicon plasma thruster
M Magarotto, M Manente, F Trezzolani… - IEEE Transactions on …, 2020 - ieeexplore.ieee.org
This article is devoted to the presentation of a numerical model of a Helicon Plasma Thruster
(HPT) which relies on: 1) the 3-D adVanced fluId dRifT diffUsion plaSma solver (3D …
(HPT) which relies on: 1) the 3-D adVanced fluId dRifT diffUsion plaSma solver (3D …
Magnetized fluid electron model within a two-dimensional hybrid simulation code for electrodeless plasma thrusters
J Zhou, A Domínguez-Vázquez… - … Sources Science and …, 2022 - iopscience.iop.org
An axisymmetric fluid model for weakly-collisional, magnetized electrons is introduced and
coupled to a particle-in-cell model for heavy species to simulate electrodeless plasma …
coupled to a particle-in-cell model for heavy species to simulate electrodeless plasma …
Numerical suite for cathodeless plasma thrusters
This work focuses on a numerical suite targeted at cathodeless plasma thrusters. A Global
Model is used for preliminary estimation of the propulsive performance. In the plasma …
Model is used for preliminary estimation of the propulsive performance. In the plasma …
Parametric study of a cathode-less radio frequency thruster
M Magarotto, D Pavarin - IEEE Transactions on Plasma …, 2020 - ieeexplore.ieee.org
A cathode-less radio frequency (RF) thruster is a plasma-based system for space
propulsion. It consists on a source for plasma generation driven by an RF antenna and a …
propulsion. It consists on a source for plasma generation driven by an RF antenna and a …
Semi-analytical model of a helicon plasma thruster
This article is devoted to the presentation of a semianalytical model of a helicon plasma
thruster based on: 1) a 0-D global source model (GSM) for the simulation of the plasma …
thruster based on: 1) a 0-D global source model (GSM) for the simulation of the plasma …