Development of a model for the near-exit plume of a Hall thruster
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.
| Main Author: | |
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| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2007
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| Online Access: | http://hdl.handle.net/1721.1/38651 |
| _version_ | 1811087566734098432 |
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| author | Parra Díaz, Félix Ignacio |
| author2 | Manuel Martínez-Sánchez. |
| author_facet | Manuel Martínez-Sánchez. Parra Díaz, Félix Ignacio |
| author_sort | Parra Díaz, Félix Ignacio |
| collection | MIT |
| description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007. |
| first_indexed | 2024-09-23T13:48:07Z |
| format | Thesis |
| id | mit-1721.1/38651 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T13:48:07Z |
| publishDate | 2007 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/386512019-04-11T11:03:49Z Development of a model for the near-exit plume of a Hall thruster Parra Díaz, Félix Ignacio Manuel Martínez-Sánchez. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007. Includes bibliographical references (leaves 77-79). This thesis presents a fluid model for electron behavior in the near-exit plume of a Hall thruster. The model provides 3D results and allows to study the azimuthal asymmetry induced by the hollow cathode. The model is composed by the charge and energy conservation equations and is intended to solve for the electrostatic potential and the electron temperature. It relies on the results of an external model for the ion behavior. The fluid equations are diffusive and are justified in the limit of small electron Larmor radius. They include the Hall transport, which is usually ignored in 2D approaches due to symmetry. The transport along magnetic field lines is high enough to convert the 3D problem into a 2D problem, where only the directions perpendicular to the magnetic field matter. In such a 2D formulation, the basic structure of the solution for the potential is studied analytically, with the result that the lines of constant potential can be approximately predicted. The potential can be found numerically after transforming the charge conservation equation into a convective-diffusive equation. The numerical results agree approximately with analytical predictions. The results suggest that the asymmetry induced by the hollow cathode mainly depend on how much the cathode perturbs the plasma density distribution. by Félix Ignacio Parra Díaz. S.M. 2007-08-29T20:39:57Z 2007-08-29T20:39:57Z 2007 2007 Thesis http://hdl.handle.net/1721.1/38651 163164953 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 79 leaves application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. Parra Díaz, Félix Ignacio Development of a model for the near-exit plume of a Hall thruster |
| title | Development of a model for the near-exit plume of a Hall thruster |
| title_full | Development of a model for the near-exit plume of a Hall thruster |
| title_fullStr | Development of a model for the near-exit plume of a Hall thruster |
| title_full_unstemmed | Development of a model for the near-exit plume of a Hall thruster |
| title_short | Development of a model for the near-exit plume of a Hall thruster |
| title_sort | development of a model for the near exit plume of a hall thruster |
| topic | Aeronautics and Astronautics. |
| url | http://hdl.handle.net/1721.1/38651 |
| work_keys_str_mv | AT parradiazfelixignacio developmentofamodelforthenearexitplumeofahallthruster |