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 …

Hall-effect thrusters for deep-space missions: A review

A Bapat, PB Salunkhe, AV Patil - IEEE Transactions on Plasma …, 2022 - ieeexplore.ieee.org
For several decades, Hall-effect thrusters (HETs) are being used in several applications,
such as orbiting satellites, deep space missions, etc. This article studies the effect of several …

A two-dimensional hybrid model of the Hall thruster discharge

FI Parra, E Ahedo, JM Fife… - Journal of Applied …, 2006 - pubs.aip.org
Particle-in-cell methods are used for ions and neutrals. Probabilistic methods are
implemented for ionization, charge-exchange collisions, gas injection, and particle-wall …

Low-frequency model of breathing oscillations in Hall discharges

S Barral, E Ahedo - Physical Review E—Statistical, Nonlinear, and Soft …, 2009 - APS
A paradigm for Hall discharge modeling is presented whereby only the time scale of the
lowest-frequency mode is explicitly resolved. The ability of such a low-frequency model to …

Effects of the radial plasma-wall interaction on the Hall thruster discharge

E Ahedo, JM Gallardo, M Martınez-Sánchez - Physics of Plasmas, 2003 - pubs.aip.org
The interaction of the plasma discharge with the ceramic walls of a Hall thruster leads to
plasma recombination, energy losses, and extra electron collisionality. These three …

Electron-wall interaction in Hall thrusters

Y Raitses, D Staack, M Keidar, NJ Fisch - Physics of Plasmas, 2005 - pubs.aip.org
Electron-wall interaction effects in Hall thrusters are studied through measurements of the
plasma response to variations of the thruster channel width and the discharge voltage. The …

Absence of Debye sheaths due to secondary electron emission

MD Campanell, AV Khrabrov, ID Kaganovich - Physical review letters, 2012 - APS
A bounded plasma where the hot electrons impacting the walls produce more than one
secondary on average is studied via particle-in-cell simulation. It is found that no classical …

Investigation of low discharge voltage Hall thruster characteristics and evaluation of loss mechanisms

DL Brown - 2009 - search.proquest.com
During the early development stages of Hall thruster technology, plasma research and
propulsion advancements centered primarily on 300-V, 1600-s specific impulse operation …

General Cause of Sheath Instability Identified for Low Collisionality Plasmas in Devices<? format?> with Secondary Electron Emission

MD Campanell, AV Khrabrov, ID Kaganovich - Physical review letters, 2012 - APS
A condition for sheath instability due to secondary electron emission (SEE) is derived for low
collisionality plasmas. When the SEE coefficient of the electrons bordering the depleted loss …

Methodology and historical perspective of a Hall thruster efficiency analysis

DL Brown, CW Larson, BE Beal… - Journal of Propulsion and …, 2009 - arc.aiaa.org
STANDARDIZATION of experimental methods, facilities, diag-nostic apparatus, and
efficiency analysis has previously been proposed in the electric propulsion community [1] …