Temperature and Density Profile of Xe I and Xe II Inside the Discharge Channel of a Hall Effect Thruster
ORAL
Abstract
Plasma species transport inside the discharge channel, specifically in the ionization and acceleration zones of a Hall Effect Thruster is the key factor that involves with thruster’s efficiency and lifetime. Spatially resolving the ionization and acceleration zones requires temperature and density profiles of neutrals and ions. A Laser Induced Fluorescence (LIF) technique is employed to determine the excited state temperature and relative density of Xe I, Xe II in different discharge conditions. Spatially distributed plasma potential maps are estimated from the top of the anode to the plume of the thruster.
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Presenters
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Mustafizur Rahman
The University of Alabama
Authors
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Mustafizur Rahman
The University of Alabama
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Richard Branam
Associate Professor, Aerospace Engineering and Mechanics, The University of Alabama, Tuscaloosa, The University of Alabama, University of Alabama