Growth of Rayleigh instability in a Hall thruster channel having dust in exit region

In a Hall thruster, the axial movement of ions towards the exit of the chamber and the divergence of ion beam sputter the wall and thus the maximum erosion of wall of the exit region takes place. This way the dust is generated, which is largely confined near the exit of the channel. By considering d...

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Main Authors: Hitendra K. Malik, Jasvendra Tyagi, Dimple Sharma
Format: Article
Language:English
Published: AIP Publishing LLC 2019-05-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/1.5050688
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author Hitendra K. Malik
Jasvendra Tyagi
Dimple Sharma
author_facet Hitendra K. Malik
Jasvendra Tyagi
Dimple Sharma
author_sort Hitendra K. Malik
collection DOAJ
description In a Hall thruster, the axial movement of ions towards the exit of the chamber and the divergence of ion beam sputter the wall and thus the maximum erosion of wall of the exit region takes place. This way the dust is generated, which is largely confined near the exit of the channel. By considering dust particles with negative charge, we derive and solve the dispersion equation for the growth of Rayleigh instability in the thruster plasma and examine its growth rate for different density, charge, mass and temperature of the dust particles. We also talk about the role of density gradient scale length on the growth of the instability.
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spelling doaj.art-ab288ef546714bd7886fd430fdbdac8f2022-12-21T23:24:42ZengAIP Publishing LLCAIP Advances2158-32262019-05-0195055220055220-510.1063/1.5050688007810ADVGrowth of Rayleigh instability in a Hall thruster channel having dust in exit regionHitendra K. Malik0Jasvendra Tyagi1Dimple Sharma2Plasma Waves and Particle Acceleration Laboratory, Department of Physics, Indian Institute of Technology Delhi, New Delhi 110 016, IndiaPlasma Waves and Particle Acceleration Laboratory, Department of Physics, Indian Institute of Technology Delhi, New Delhi 110 016, IndiaPlasma Waves and Particle Acceleration Laboratory, Department of Physics, Indian Institute of Technology Delhi, New Delhi 110 016, IndiaIn a Hall thruster, the axial movement of ions towards the exit of the chamber and the divergence of ion beam sputter the wall and thus the maximum erosion of wall of the exit region takes place. This way the dust is generated, which is largely confined near the exit of the channel. By considering dust particles with negative charge, we derive and solve the dispersion equation for the growth of Rayleigh instability in the thruster plasma and examine its growth rate for different density, charge, mass and temperature of the dust particles. We also talk about the role of density gradient scale length on the growth of the instability.http://dx.doi.org/10.1063/1.5050688
spellingShingle Hitendra K. Malik
Jasvendra Tyagi
Dimple Sharma
Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
AIP Advances
title Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
title_full Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
title_fullStr Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
title_full_unstemmed Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
title_short Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
title_sort growth of rayleigh instability in a hall thruster channel having dust in exit region
url http://dx.doi.org/10.1063/1.5050688
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