Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters

Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, February 1999. === Includes bibliographical references (p. 263-268). === In order to study the physics of the acceleration process in Hall thrusters, an evolved hybrid particle-in-cell (PIC) numerical model...

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Main Author: Fife, John Michael
Other Authors: Manuel Martinez-Sanchez.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://hdl.handle.net/1721.1/9732
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spelling ndltd-MIT-oai-dspace.mit.edu-1721.1-97322020-07-15T07:09:31Z Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters Hybrid particle-in-cell modeling and electrostatic probe survey of Hall thrusters Fife, John Michael Manuel Martinez-Sanchez. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics Aeronautics and Astronautics Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, February 1999. Includes bibliographical references (p. 263-268). In order to study the physics of the acceleration process in Hall thrusters, an evolved hybrid particle-in-cell (PIC) numerical model was developed. A set of quasi-one-dimensional fluid equations are used for electrons, and a particle-tracking Boltzmann solver is used for the heavy species. The two solutions are linked by charge neutrality. A novel statistical approach to particle creation and tracking is employed which reduces computational time. To provide boundary conditions for the numerical model, and to verify its accuracy, an extensive set of electrostatic probe measurements were performed in the plume of an SPT- 70. Various probe geometries were used, including triple probes, to measure the time­averaged plasma parameters in the near-plume. Also, AC components of discharge current and floating potential were measured. The combined experimental and numerical results are used to examine phenomena such as the nature of low-frequency discharge oscillations, the interaction of the thruster walls with the plasma, the distribution of ion energies ejected from the thruster, and the effect on efficiency of facility background pressure. Performance results from the numerical model agree well with measurements. A formula for the change in measured efficiency versus facility pressure is also presented, based on numerical results. Widening of the ion distribution of energies is seen, and attributed to time variation of the electric field, due to oscillations. Measured low-frequency oscillations seem to be related to an ionization instability observed in the numerical model, but conclusive evidence is not found. Although the model predicts strong electric fields outside the acceleration channel, experiments do not. The discrepancy is believed to be due to localized anomalous electron conductivity caused by azimuthal asymmetry. by John Michale Fife. Ph.D. 2005-08-19T19:47:30Z 2005-08-19T19:47:30Z 1998 1999 Thesis http://hdl.handle.net/1721.1/9732 42697272 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 268 p. 16626187 bytes 16625944 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
collection NDLTD
language English
format Others
sources NDLTD
topic Aeronautics and Astronautics
spellingShingle Aeronautics and Astronautics
Fife, John Michael
Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
description Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, February 1999. === Includes bibliographical references (p. 263-268). === In order to study the physics of the acceleration process in Hall thrusters, an evolved hybrid particle-in-cell (PIC) numerical model was developed. A set of quasi-one-dimensional fluid equations are used for electrons, and a particle-tracking Boltzmann solver is used for the heavy species. The two solutions are linked by charge neutrality. A novel statistical approach to particle creation and tracking is employed which reduces computational time. To provide boundary conditions for the numerical model, and to verify its accuracy, an extensive set of electrostatic probe measurements were performed in the plume of an SPT- 70. Various probe geometries were used, including triple probes, to measure the time­averaged plasma parameters in the near-plume. Also, AC components of discharge current and floating potential were measured. The combined experimental and numerical results are used to examine phenomena such as the nature of low-frequency discharge oscillations, the interaction of the thruster walls with the plasma, the distribution of ion energies ejected from the thruster, and the effect on efficiency of facility background pressure. Performance results from the numerical model agree well with measurements. A formula for the change in measured efficiency versus facility pressure is also presented, based on numerical results. Widening of the ion distribution of energies is seen, and attributed to time variation of the electric field, due to oscillations. Measured low-frequency oscillations seem to be related to an ionization instability observed in the numerical model, but conclusive evidence is not found. Although the model predicts strong electric fields outside the acceleration channel, experiments do not. The discrepancy is believed to be due to localized anomalous electron conductivity caused by azimuthal asymmetry. === by John Michale Fife. === Ph.D.
author2 Manuel Martinez-Sanchez.
author_facet Manuel Martinez-Sanchez.
Fife, John Michael
author Fife, John Michael
author_sort Fife, John Michael
title Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
title_short Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
title_full Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
title_fullStr Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
title_full_unstemmed Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters
title_sort hybrid-pic modeling and electrostatic probe survey of hall thrusters
publisher Massachusetts Institute of Technology
publishDate 2005
url http://hdl.handle.net/1721.1/9732
work_keys_str_mv AT fifejohnmichael hybridpicmodelingandelectrostaticprobesurveyofhallthrusters
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