[HTML][HTML] Space micropropulsion systems for Cubesats and small satellites: From proximate targets to furthermost frontiers

I Levchenko, K Bazaka, Y Ding, Y Raitses… - Applied Physics …, 2018 - pubs.aip.org
Rapid evolution of miniaturized, automatic, robotized, function-centered devices has
redefined space technology, bringing closer the realization of most ambitious interplanetary …

Latest progress in Hall thrusters plasma modelling

F Taccogna, L Garrigues - Reviews of Modern Plasma Physics, 2019 - Springer
In the last 30 years, numerical models have revealed different physical mechanisms
involved in the Hall thruster functioning leading to a bridge between analytical …

Similarity theory and scaling laws for low-temperature plasma discharges: A comprehensive review

Y Fu, H Wang, X Wang - Reviews of Modern Plasma Physics, 2023 - Springer
Similarity theory and scaling laws determine how physical laws remain the same when
control parameters are changed, which is essential for the correlation, prediction, and …

Plasma propulsion modeling with particle-based algorithms

F Taccogna, F Cichocki, D Eremin, G Fubiani… - Journal of Applied …, 2023 - pubs.aip.org
This Perspective paper deals with an overview of particle-in-cell/Monte Carlo collision
models applied to different plasma-propulsion configurations and scenarios, from …

Concept of the generalized reduced-order particle-in-cell scheme and verification in an axial-azimuthal Hall thruster configuration

M Reza, F Faraji, A Knoll - Journal of Physics D: Applied Physics, 2023 - iopscience.iop.org
The reduced-order particle-in-cell (PIC) scheme is a novel modeling approach that enables
computationally efficient electrostatic kinetic simulations of plasma. In our previous …

Full particle-in-cell simulation methodology for axisymmetric Hall effect thrusters

J Szabo, N Warner, M Martinez-Sanchez… - Journal of Propulsion …, 2014 - arc.aiaa.org
A fully kinetic plasma simulation based upon the particle-in-cell and Monte Carlo collision
methodologies was developed to model axisymmetric closed-drift Hall effect thruster …

Kinetic particle simulation of discharge and wall erosion of a Hall thruster

S Cho, K Komurasaki, Y Arakawa - Physics of Plasmas, 2013 - pubs.aip.org
The primary lifetime limiting factor of Hall thrusters is the wall erosion caused by the ion
induced sputtering, which is predominated by dielectric wall sheath and pre-sheath …

Kinetic simulations of a plasma thruster

F Taccogna, R Schneider, S Longo… - … Sources Science and …, 2008 - iopscience.iop.org
The modelling of the Hall thruster SPT-100 is a very important issue in view of the increasing
importance of such propulsion devices in space applications. Only kinetic models can …

Three-dimensional particle-in-cell model of Hall thruster: The discharge channel

F Taccogna, P Minelli - Physics of Plasmas, 2018 - pubs.aip.org
There are still many missing elements to complete the physical picture at the basis of the
Hall thruster functioning. The origin of the anomalous electron cross-field transport often …

Generalized reduced-order particle-in-cell scheme for Hall thruster modeling: concept and in-depth verification in the axial-azimuthal configuration

M Reza, F Faraji, A Knoll - arXiv preprint arXiv:2208.13106, 2022 - arxiv.org
Reduced-order particle-in-cell (PIC) scheme is a novel modeling approach that enables
computationally efficient electrostatic kinetic simulations of plasma. In our previous …