[HTML][HTML] Physics of E× B discharges relevant to plasma propulsion and similar technologies

ID Kaganovich, A Smolyakov, Y Raitses, E Ahedo… - Physics of …, 2020 - pubs.aip.org
This paper provides perspectives on recent progress in understanding the physics of
devices in which the external magnetic field is applied perpendicular to the discharge …

Plasma mass separation in configuration with potential well

G Liziakin, N Antonov, VS Smirnov… - Journal of Physics D …, 2021 - iopscience.iop.org
The details of the charged particle separation by mass in the configuration with axial
magnetic and radial electric fields are studied. The radial electric field, oriented to the …

Characterization of hollow cathode plasma turbulence using coherent Thomson scattering

S Tsikata, K Hara, S Mazouffre - Journal of Applied Physics, 2021 - pubs.aip.org
Turbulence in hollow cathodes used for space propulsion is believed to play an important
role in anomalous electron transport and ion heating. In this work, the implementation of …

[HTML][HTML] Far-field plume characterization of a low-power cylindrical Hall thruster

T Perrotin, AE Vinci, S Mazouffre, P Fajardo… - Journal of Applied …, 2024 - pubs.aip.org
A fully cylindrical Hall thruster prototype was tested in the power range of 30–300 W with the
objective of understanding the behavior of the discharge as a function of input parameters …

Phenomenological plasma model for open-end emitter with orificed keeper hollow cathodes

GC Potrivitu, S Xu - Acta Astronautica, 2022 - Elsevier
Hollow cathodes are used as thermionic emitters in a variety of electric propulsion devices
such as the Hall thruster. This work studies the derivation and discusses the results of a …

A low-current LaB6 open-end knife-edge emitter hollow cathode for low-power Hall thrusters

GC Potrivitu, L Xu, S Xu - Plasma Sources Science and …, 2021 - iopscience.iop.org
Heated thermionic cathodes based on LaB 6 emitters are known to consume a relatively
large amount of power during the heating part of the ignition phase. Miniaturized electric …

Characterization of electron mach number in a hollow cathode with Thomson scattering

PJ Roberts, B Jorns - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0843. vid Electron flow is
measured non-perturbatively via the incoherent scattering of laser light from electrons in a …

Discharge and plasma plume characterization of a 100 A-class LaB6 hollow cathode

S Mazouffre, R Joussot, B Vincent… - Journal of Applied …, 2021 - pubs.aip.org
This article reports on the characterization of a laboratory model 100 A-class hollow cathode
with a sintered lanthanum hexaboride (⁠ LaB 6⁠) emitter for high-power Hall thrusters. The …

[HTML][HTML] A global model for evaluating discharge characteristics and performance of hollow cathodes

T Feng, M Long, XIA Qimeng, WU Zhiwen… - Chinese Journal of …, 2024 - Elsevier
Hollow cathode, with the highest plasma density, current density, and temperature, becomes
one of the most important components in the electro-thruster system. As the electric …

[PDF][PDF] Zero-dimensional plasma model for open-end emitter thermionic hollow cathodes with integrated thermal model

GC Potrivitu, M Laterza, M Ridzuan… - … , IEPC-2022-116 …, 2022 - researchgate.net
V volume/potential, m− 3 or V Greek η resistivity, Ω· m σ cross section, m2 φ potential, V or
eV Subscript/Superscript ck cathode-keeper d discharge ds double sheath e electron ef f …