Improving Hall Thruster Plume Simulation through Refined Characterization ofNear-field Plasma Properties.

Hall Thruster Modeling;Aerospace Engineering;Engineering;Aerospace Science

Huismann, Tyler D.Thomas, Alexander George Roy ;

University of Michigan

关键词: Hall Thruster Modeling;    Aerospace Engineering;    Engineering;    Aerospace Science;   

Others  :  https://deepblue.lib.umich.edu/bitstream/handle/2027.42/89770/huismann_1.pdf?sequence=1&isAllowed=y

瑞士|英语

来源: The Illinois Digital Environment for Access to Learning and Scholarship

【 摘 要 】

Due to the rapidly expanding role of electric propulsion (EP) devices, it is important to evaluate their integration with other spacecraft systems.Specifically, EP device plumes can play a major role in spacecraft integration, and as such, accurate characterization of plume structure bears on mission success.This dissertation addresses issues related to accurate prediction of plume structure in a particular type of EP device, a Hall thruster.This is done in two ways:first, by coupling current plume simulation models with current models that simulate a Hall thruster;;s internal plasma behavior; second, by improving plume simulation models and thereby increasing physical fidelity.These methods are assessed by comparing simulated results to experimental measurements.Assessment indicates the two methods improve plume modeling capabilities significantly:using far-field ion current density as a metric, these approaches used in conjunction improve agreement with measurements by a factor of 2.5, as compared to previous methods.Based on comparison to experimental measurements, recent computational work on discharge chamber modeling has been largely successful in predicting properties of internal thruster plasmas.This model can provide detailed information on plasma properties at a variety of locations.Frequently, experimental data is not available at many locations that are of interest regarding computational models.Excepting the presence of experimental data, there are limited alternatives for scientifically determining plasma properties that are necessary as inputs into plume simulations.Therefore, this dissertation focuses on coupling current models that simulate internal thruster plasma behavior with plume simulation models.Further, recent experimental work on atom-ion interactions has provided a better understanding of particle collisions within plasmas.This experimental work is used to update collision models in a current plume simulation code.Previous versions of the code assume an unknown dependence between particles;; pre-collision velocities and post-collision scattering angles.This dissertation focuses on updating several of these types of collisions by assuming a curve fit based on the measurements of atom-ion interactions, such that previously unknown angular dependences are well-characterized.