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You searched for subject:(Hall thruster). Showing records 1 – 30 of 61 total matches.

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Cal Poly

1. Barlog, Christopher M. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  High Efficiency Multistage Plasma Thrusters (HEMPTs) are a relatively new form of electric propulsion that show promise for use on a variety of missions… (more)

Subjects/Keywords: HEMPT; EP; Electric Propulsion; Magnetic Field; Thruster; Hall Thruster; Ion Thruster; Propulsion and Power

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APA (6th Edition):

Barlog, C. M. (2015). Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179

Chicago Manual of Style (16th Edition):

Barlog, Christopher M. “Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.” 2015. Masters Thesis, Cal Poly. Accessed March 07, 2021. https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179.

MLA Handbook (7th Edition):

Barlog, Christopher M. “Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.” 2015. Web. 07 Mar 2021.

Vancouver:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2021 Mar 07]. Available from: https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179.

Council of Science Editors:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179


University of Michigan

2. Huismann, Tyler D. Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties.

Degree: PhD, Aerospace Science, 2011, University of Michigan

 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… (more)

Subjects/Keywords: Hall Thruster Modeling; Aerospace Engineering; Engineering

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APA (6th Edition):

Huismann, T. D. (2011). Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/89770

Chicago Manual of Style (16th Edition):

Huismann, Tyler D. “Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties.” 2011. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/89770.

MLA Handbook (7th Edition):

Huismann, Tyler D. “Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties.” 2011. Web. 07 Mar 2021.

Vancouver:

Huismann TD. Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/89770.

Council of Science Editors:

Huismann TD. Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/89770


Universidade de Brasília

3. João Henrique Campos de Souza. Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes.

Degree: 2006, Universidade de Brasília

Since 2000, The Plasma Laboratory of the Physics Institute of the University of Brasília (LP) has developed the Project PHALL, with the objectives to develop… (more)

Subjects/Keywords: FISICA; Hall Thruster; Plasma; Plasma (Gases ionizados)

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APA (6th Edition):

Souza, J. H. C. d. (2006). Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes. (Thesis). Universidade de Brasília. Retrieved from http://bdtd.bce.unb.br/tedesimplificado/tde_busca/arquivo.php?codArquivo=1844

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Souza, João Henrique Campos de. “Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes.” 2006. Thesis, Universidade de Brasília. Accessed March 07, 2021. http://bdtd.bce.unb.br/tedesimplificado/tde_busca/arquivo.php?codArquivo=1844.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Souza, João Henrique Campos de. “Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes.” 2006. Web. 07 Mar 2021.

Vancouver:

Souza JHCd. Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes. [Internet] [Thesis]. Universidade de Brasília; 2006. [cited 2021 Mar 07]. Available from: http://bdtd.bce.unb.br/tedesimplificado/tde_busca/arquivo.php?codArquivo=1844.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Souza JHCd. Estudo da Dinâmica de Partículas em um Propulsor a Plasma do tipo Hall com Ímãs Permanentes. [Thesis]. Universidade de Brasília; 2006. Available from: http://bdtd.bce.unb.br/tedesimplificado/tde_busca/arquivo.php?codArquivo=1844

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

4. Pigeon, Carl. Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites.

Degree: 2017, University of Toronto

To enable more advanced commercial microsatellite missions, a low power electric propulsion system was designed by the University of Toronto Space Flight Laboratory. A prototype… (more)

Subjects/Keywords: Electric Propulsion; Hall Thruster; Microsatellite; Plasma; 0538

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APA (6th Edition):

Pigeon, C. (2017). Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79066

Chicago Manual of Style (16th Edition):

Pigeon, Carl. “Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites.” 2017. Masters Thesis, University of Toronto. Accessed March 07, 2021. http://hdl.handle.net/1807/79066.

MLA Handbook (7th Edition):

Pigeon, Carl. “Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites.” 2017. Web. 07 Mar 2021.

Vancouver:

Pigeon C. Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1807/79066.

Council of Science Editors:

Pigeon C. Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79066


Colorado State University

5. Andreano, Thomas Malachi. Performance and plume characterization of a laboratory krypton Hall thruster.

Degree: MS(M.S.), Mechanical Engineering, 2020, Colorado State University

Hall thruster research has been in progress at the CSU Electric Propulsion and Plasma Engineering (CEPPE) lab for the past decade, however, a full performance… (more)

Subjects/Keywords: Hall thruster; propulsion; electric propulsion; space; plasma

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APA (6th Edition):

Andreano, T. M. (2020). Performance and plume characterization of a laboratory krypton Hall thruster. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/208509

Chicago Manual of Style (16th Edition):

Andreano, Thomas Malachi. “Performance and plume characterization of a laboratory krypton Hall thruster.” 2020. Masters Thesis, Colorado State University. Accessed March 07, 2021. http://hdl.handle.net/10217/208509.

MLA Handbook (7th Edition):

Andreano, Thomas Malachi. “Performance and plume characterization of a laboratory krypton Hall thruster.” 2020. Web. 07 Mar 2021.

Vancouver:

Andreano TM. Performance and plume characterization of a laboratory krypton Hall thruster. [Internet] [Masters thesis]. Colorado State University; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10217/208509.

Council of Science Editors:

Andreano TM. Performance and plume characterization of a laboratory krypton Hall thruster. [Masters Thesis]. Colorado State University; 2020. Available from: http://hdl.handle.net/10217/208509


Michigan Technological University

6. Vanheusden, Elizabeth M. Thermomagnetic Convective Cooling of Hall Effect Thruster.

Degree: MS, Department of Mechanical Engineering-Engineering Mechanics, 2018, Michigan Technological University

  This work proposes and shows that thermomagnetic convection could be used in zero gravity to cool components of a Hall-effect thruster. A ferrofluid cavity… (more)

Subjects/Keywords: ferrofluids; thermomagnetic; convection; hall effect thruster; hall-effect thruster; Heat Transfer, Combustion

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APA (6th Edition):

Vanheusden, E. M. (2018). Thermomagnetic Convective Cooling of Hall Effect Thruster. (Masters Thesis). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/690

Chicago Manual of Style (16th Edition):

Vanheusden, Elizabeth M. “Thermomagnetic Convective Cooling of Hall Effect Thruster.” 2018. Masters Thesis, Michigan Technological University. Accessed March 07, 2021. https://digitalcommons.mtu.edu/etdr/690.

MLA Handbook (7th Edition):

Vanheusden, Elizabeth M. “Thermomagnetic Convective Cooling of Hall Effect Thruster.” 2018. Web. 07 Mar 2021.

Vancouver:

Vanheusden EM. Thermomagnetic Convective Cooling of Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2018. [cited 2021 Mar 07]. Available from: https://digitalcommons.mtu.edu/etdr/690.

Council of Science Editors:

Vanheusden EM. Thermomagnetic Convective Cooling of Hall Effect Thruster. [Masters Thesis]. Michigan Technological University; 2018. Available from: https://digitalcommons.mtu.edu/etdr/690


Colorado State University

7. Mullins, Carl Raymond. Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A.

Degree: MS(M.S.), Mechanical Engineering, 2015, Colorado State University

 A direct, accurate method to measure thrust produced by a Hall Effect thruster on orbit does not currently exist. The ability to calculate produced thrust… (more)

Subjects/Keywords: azimuthal current; diagnostic; Hall current; Hall thruster; non-invasive

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APA (6th Edition):

Mullins, C. R. (2015). Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/170326

Chicago Manual of Style (16th Edition):

Mullins, Carl Raymond. “Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A.” 2015. Masters Thesis, Colorado State University. Accessed March 07, 2021. http://hdl.handle.net/10217/170326.

MLA Handbook (7th Edition):

Mullins, Carl Raymond. “Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A.” 2015. Web. 07 Mar 2021.

Vancouver:

Mullins CR. Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A. [Internet] [Masters thesis]. Colorado State University; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10217/170326.

Council of Science Editors:

Mullins CR. Non-invasive Hall current distribution measurement system for Hall Effect thrusters, A. [Masters Thesis]. Colorado State University; 2015. Available from: http://hdl.handle.net/10217/170326


University of Michigan

8. Dale, Ethan. Investigation of the Hall Thruster Breathing Mode.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

Hall thrusters can support a wide range of instabilities, many of which remain poorly understood yet are known to play a critical role in the… (more)

Subjects/Keywords: electric propulsion; Hall thruster; breathing mode; Aerospace Engineering; Engineering

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APA (6th Edition):

Dale, E. (2019). Investigation of the Hall Thruster Breathing Mode. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/155282

Chicago Manual of Style (16th Edition):

Dale, Ethan. “Investigation of the Hall Thruster Breathing Mode.” 2019. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/155282.

MLA Handbook (7th Edition):

Dale, Ethan. “Investigation of the Hall Thruster Breathing Mode.” 2019. Web. 07 Mar 2021.

Vancouver:

Dale E. Investigation of the Hall Thruster Breathing Mode. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/155282.

Council of Science Editors:

Dale E. Investigation of the Hall Thruster Breathing Mode. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/155282


University of Saskatchewan

9. Morin, Vincent 1992-. Sheath Boundary Effects on the Stability of Hall Plasmas.

Degree: 2018, University of Saskatchewan

 Plasma devices based on the ExB- field con figuration (where the externally applied electric and magnetic fields are everywhere perpendicular) are used for a variety… (more)

Subjects/Keywords: Plasma; instability; transport; Hall thruster; Penning trap; magnetron; sheath

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APA (6th Edition):

Morin, V. 1. (2018). Sheath Boundary Effects on the Stability of Hall Plasmas. (Thesis). University of Saskatchewan. Retrieved from http://hdl.handle.net/10388/10726

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Morin, Vincent 1992-. “Sheath Boundary Effects on the Stability of Hall Plasmas.” 2018. Thesis, University of Saskatchewan. Accessed March 07, 2021. http://hdl.handle.net/10388/10726.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Morin, Vincent 1992-. “Sheath Boundary Effects on the Stability of Hall Plasmas.” 2018. Web. 07 Mar 2021.

Vancouver:

Morin V1. Sheath Boundary Effects on the Stability of Hall Plasmas. [Internet] [Thesis]. University of Saskatchewan; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10388/10726.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Morin V1. Sheath Boundary Effects on the Stability of Hall Plasmas. [Thesis]. University of Saskatchewan; 2018. Available from: http://hdl.handle.net/10388/10726

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Colorado State University

10. Rath, Jordan L. Laser diagnostic methods for plasma sheath potential mapping and electric field measurement.

Degree: MS(M.S.), Mechanical Engineering, 2013, Colorado State University

 This thesis presents the development of two laser diagnostic approaches for electric field measurements in plasmas and gases. Hall effect thrusters, and other electric propulsion… (more)

Subjects/Keywords: sheath; optics; polarimetry; plasma; Hall thruster; laser induced fluorescence

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APA (6th Edition):

Rath, J. L. (2013). Laser diagnostic methods for plasma sheath potential mapping and electric field measurement. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/81070

Chicago Manual of Style (16th Edition):

Rath, Jordan L. “Laser diagnostic methods for plasma sheath potential mapping and electric field measurement.” 2013. Masters Thesis, Colorado State University. Accessed March 07, 2021. http://hdl.handle.net/10217/81070.

MLA Handbook (7th Edition):

Rath, Jordan L. “Laser diagnostic methods for plasma sheath potential mapping and electric field measurement.” 2013. Web. 07 Mar 2021.

Vancouver:

Rath JL. Laser diagnostic methods for plasma sheath potential mapping and electric field measurement. [Internet] [Masters thesis]. Colorado State University; 2013. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10217/81070.

Council of Science Editors:

Rath JL. Laser diagnostic methods for plasma sheath potential mapping and electric field measurement. [Masters Thesis]. Colorado State University; 2013. Available from: http://hdl.handle.net/10217/81070


Colorado State University

11. Tao, Lei. Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement.

Degree: PhD, Mechanical Engineering, 2011, Colorado State University

Hall thruster and other Electric propulsion (EP) devices have become appealing alternatives to traditional chemical propulsion thrusters for space applications due to this high specific… (more)

Subjects/Keywords: boron nitride; Hall thruster; erosion; cavity ring down spectroscopy

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APA (6th Edition):

Tao, L. (2011). Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement. (Doctoral Dissertation). Colorado State University. Retrieved from http://hdl.handle.net/10217/50162

Chicago Manual of Style (16th Edition):

Tao, Lei. “Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement.” 2011. Doctoral Dissertation, Colorado State University. Accessed March 07, 2021. http://hdl.handle.net/10217/50162.

MLA Handbook (7th Edition):

Tao, Lei. “Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement.” 2011. Web. 07 Mar 2021.

Vancouver:

Tao L. Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement. [Internet] [Doctoral dissertation]. Colorado State University; 2011. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10217/50162.

Council of Science Editors:

Tao L. Continuous-wave cavity ring down spectroscopy sensor for Hall thruster erosion measurement. [Doctoral Dissertation]. Colorado State University; 2011. Available from: http://hdl.handle.net/10217/50162


University of Toronto

12. Svatos, Adam Ladislav. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.

Degree: 2017, University of Toronto

This thesis describes the author's contributions to three separate projects. The bus of the NORSAT-2 satellite was developed by the Space Flight Laboratory (SFL) for… (more)

Subjects/Keywords: electronic; Hall effect; power; propulsion; space; thruster; 0538

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APA (6th Edition):

Svatos, A. L. (2017). Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79053

Chicago Manual of Style (16th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Masters Thesis, University of Toronto. Accessed March 07, 2021. http://hdl.handle.net/1807/79053.

MLA Handbook (7th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Web. 07 Mar 2021.

Vancouver:

Svatos AL. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1807/79053.

Council of Science Editors:

Svatos AL. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79053


Michigan Technological University

13. Slabaugh, Tristan. Cathode Coupling in a Low Power Hall Effect Thruster.

Degree: MS, Department of Mechanical Engineering-Engineering Mechanics, 2019, Michigan Technological University

  This work explores the effects of cathode position on Orbion Space Technology’s Aurora thruster performance and ignition characteristics. The cathode was moved to points… (more)

Subjects/Keywords: Hall effect thruster; Cathode Coupling; Propulsion and Power

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APA (6th Edition):

Slabaugh, T. (2019). Cathode Coupling in a Low Power Hall Effect Thruster. (Masters Thesis). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/886

Chicago Manual of Style (16th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Masters Thesis, Michigan Technological University. Accessed March 07, 2021. https://digitalcommons.mtu.edu/etdr/886.

MLA Handbook (7th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Web. 07 Mar 2021.

Vancouver:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2019. [cited 2021 Mar 07]. Available from: https://digitalcommons.mtu.edu/etdr/886.

Council of Science Editors:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Masters Thesis]. Michigan Technological University; 2019. Available from: https://digitalcommons.mtu.edu/etdr/886


University of Michigan

14. Huang, Wensheng. Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics.

Degree: PhD, Aerospace Engineering, 2011, University of Michigan

 This dissertation describes the use of optical diagnostics to study the Hall thruster channel wall erosion problem. The novel use of two-axis laser-induced fluorescence velocimetry… (more)

Subjects/Keywords: Hall Thruster; Channel Wall Erosion; Optical Diagnostics; LIF; CRDS; Aerospace Engineering; Engineering

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APA (6th Edition):

Huang, W. (2011). Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/86567

Chicago Manual of Style (16th Edition):

Huang, Wensheng. “Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics.” 2011. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/86567.

MLA Handbook (7th Edition):

Huang, Wensheng. “Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics.” 2011. Web. 07 Mar 2021.

Vancouver:

Huang W. Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/86567.

Council of Science Editors:

Huang W. Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/86567


Texas A&M University

15. Greve, Christine Marie. The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications.

Degree: MS, Aerospace Engineering, 2019, Texas A&M University

 The development and subsequent studies regarding statistical convergence for a data-driven calibration approach to physics-based models are presented with the ultimate goal of using the… (more)

Subjects/Keywords: plasma physics; data-driven model; machine learning; Hall effect thruster; model calibration

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APA (6th Edition):

Greve, C. M. (2019). The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188739

Chicago Manual of Style (16th Edition):

Greve, Christine Marie. “The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications.” 2019. Masters Thesis, Texas A&M University. Accessed March 07, 2021. http://hdl.handle.net/1969.1/188739.

MLA Handbook (7th Edition):

Greve, Christine Marie. “The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications.” 2019. Web. 07 Mar 2021.

Vancouver:

Greve CM. The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications. [Internet] [Masters thesis]. Texas A&M University; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1969.1/188739.

Council of Science Editors:

Greve CM. The Development of a Data-Driven Model Calibration Method for Plasma Physics Applications. [Masters Thesis]. Texas A&M University; 2019. Available from: http://hdl.handle.net/1969.1/188739


Colorado State University

16. Morozko, Zoe. Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster.

Degree: MS(M.S.), Mechanical Engineering, 2013, Colorado State University

 A Hall thruster is an electric propulsion device that produces thrust electrostatically by accelerating propellant to velocities 5 to 10 times higher than is achievable… (more)

Subjects/Keywords: electric propulsion; Hall thruster; magnetic field measurement; magnetic sensors; plasma propulsion; thrust stand

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APA (6th Edition):

Morozko, Z. (2013). Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/79123

Chicago Manual of Style (16th Edition):

Morozko, Zoe. “Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster.” 2013. Masters Thesis, Colorado State University. Accessed March 07, 2021. http://hdl.handle.net/10217/79123.

MLA Handbook (7th Edition):

Morozko, Zoe. “Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster.” 2013. Web. 07 Mar 2021.

Vancouver:

Morozko Z. Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster. [Internet] [Masters thesis]. Colorado State University; 2013. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10217/79123.

Council of Science Editors:

Morozko Z. Feasibility assessment of magnetic sensors for measurement of Hall current induced changes to the static magnetic field nearby a Hall thruster. [Masters Thesis]. Colorado State University; 2013. Available from: http://hdl.handle.net/10217/79123


University of Washington

17. Jenkins, Nadiah. Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss.

Degree: 2019, University of Washington

 Breathing mode instabilities, axially-oriented waves between 5-40 kHz, have been observed in Hall thruster operation since the earliest days of experimental research, including their ability… (more)

Subjects/Keywords: breathing mode; hall thruster; numerical simulation; plasma physics; Aerospace engineering; Plasma physics; Aeronautics and astronautics

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APA (6th Edition):

Jenkins, N. (2019). Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/44008

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Jenkins, Nadiah. “Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss.” 2019. Thesis, University of Washington. Accessed March 07, 2021. http://hdl.handle.net/1773/44008.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Jenkins, Nadiah. “Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss.” 2019. Web. 07 Mar 2021.

Vancouver:

Jenkins N. Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss. [Internet] [Thesis]. University of Washington; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1773/44008.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jenkins N. Breathing Mode Effects on Hall Thruster Plasma Quantities and Channel Wall Power Loss. [Thesis]. University of Washington; 2019. Available from: http://hdl.handle.net/1773/44008

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Michigan Technological University

18. Hopkins, Mark A. EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT.

Degree: PhD, Department of Mechanical Engineering-Engineering Mechanics, 2015, Michigan Technological University

  In this study, the use of magnesium as a Hall thruster propellant was evaluated. A xenon Hall thruster was modified such that magnesium propellant… (more)

Subjects/Keywords: Condensable Propellant; Electric Propulsion; Hall Thruster; Magnesium; Space Propulsion; Plasma and Beam Physics

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APA (6th Edition):

Hopkins, M. A. (2015). EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT. (Doctoral Dissertation). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etds/903

Chicago Manual of Style (16th Edition):

Hopkins, Mark A. “EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT.” 2015. Doctoral Dissertation, Michigan Technological University. Accessed March 07, 2021. https://digitalcommons.mtu.edu/etds/903.

MLA Handbook (7th Edition):

Hopkins, Mark A. “EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT.” 2015. Web. 07 Mar 2021.

Vancouver:

Hopkins MA. EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT. [Internet] [Doctoral dissertation]. Michigan Technological University; 2015. [cited 2021 Mar 07]. Available from: https://digitalcommons.mtu.edu/etds/903.

Council of Science Editors:

Hopkins MA. EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT. [Doctoral Dissertation]. Michigan Technological University; 2015. Available from: https://digitalcommons.mtu.edu/etds/903


Virginia Tech

19. Spicer, Randy Lee. Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data.

Degree: MS, Aerospace Engineering, 2007, Virginia Tech

 This thesis discusses the recent developments to the electric propulsion plume code DRACO as well as a validation and sensitivity analysis of the code using… (more)

Subjects/Keywords: Hall Thruster; DRACO; PIC; Electric Propulsion

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APA (6th Edition):

Spicer, R. L. (2007). Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34460

Chicago Manual of Style (16th Edition):

Spicer, Randy Lee. “Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data.” 2007. Masters Thesis, Virginia Tech. Accessed March 07, 2021. http://hdl.handle.net/10919/34460.

MLA Handbook (7th Edition):

Spicer, Randy Lee. “Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data.” 2007. Web. 07 Mar 2021.

Vancouver:

Spicer RL. Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data. [Internet] [Masters thesis]. Virginia Tech; 2007. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/10919/34460.

Council of Science Editors:

Spicer RL. Validation of the DRACO Particle-in-Cell Code using Busek 200W Hall Thruster Experimental Data. [Masters Thesis]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/34460


Cleveland State University

20. Urban, Peter J. Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster.

Degree: MSin Mechanical Engineering, Washkewicz College of Engineering, 2018, Cleveland State University

 Currently there is a large interest in the use of more efficient means of propulsion in long term missions due to the costs and difficulties… (more)

Subjects/Keywords: Engineering; Mechanical Engineering; Aerospace Engineering; plasma; hall thruster; measurement; electric propulsion; spectroscopy

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APA (6th Edition):

Urban, P. J. (2018). Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster. (Masters Thesis). Cleveland State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=csu1528216243044845

Chicago Manual of Style (16th Edition):

Urban, Peter J. “Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster.” 2018. Masters Thesis, Cleveland State University. Accessed March 07, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=csu1528216243044845.

MLA Handbook (7th Edition):

Urban, Peter J. “Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster.” 2018. Web. 07 Mar 2021.

Vancouver:

Urban PJ. Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster. [Internet] [Masters thesis]. Cleveland State University; 2018. [cited 2021 Mar 07]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1528216243044845.

Council of Science Editors:

Urban PJ. Non-Intrusive Optical Measurement of Electron Temperature in Near Field Plume of Hall Thruster. [Masters Thesis]. Cleveland State University; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1528216243044845

21. Charoy, Thomas. Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall.

Degree: Docteur es, Physique, 2020, Institut polytechnique de Paris

Ces dernières années, le nombre de satellites en orbite autour de la Terre a augmenté de manière exponentielle. Grâce à leur faible consommation en carburant,… (more)

Subjects/Keywords: Propulsion électrique; Propulseur de Hall; Simulation PIC; Benchmark; Instabilités; Electric propulsion; Hall thruster; PIC simulation; Benchmark; Instabilities; 629.465 5

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APA (6th Edition):

Charoy, T. (2020). Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall. (Doctoral Dissertation). Institut polytechnique de Paris. Retrieved from http://www.theses.fr/2020IPPAX046

Chicago Manual of Style (16th Edition):

Charoy, Thomas. “Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall.” 2020. Doctoral Dissertation, Institut polytechnique de Paris. Accessed March 07, 2021. http://www.theses.fr/2020IPPAX046.

MLA Handbook (7th Edition):

Charoy, Thomas. “Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall.” 2020. Web. 07 Mar 2021.

Vancouver:

Charoy T. Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall. [Internet] [Doctoral dissertation]. Institut polytechnique de Paris; 2020. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2020IPPAX046.

Council of Science Editors:

Charoy T. Numerical study of electron transport in Hall thrusters : Etude numérique du transport des électrons dans un propulseur à effet Hall. [Doctoral Dissertation]. Institut polytechnique de Paris; 2020. Available from: http://www.theses.fr/2020IPPAX046

22. Sadouni, Sarah. Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources.

Degree: Docteur es, Ingénierie des Plasmas, 2020, Université Toulouse III – Paul Sabatier

Il est bien connu que les plasmas froids magnétisés dans des dispositifs tels que les propulseurs Hall et les sources d'ions montrent souvent l'émergence d'instabilités… (more)

Subjects/Keywords: Modélisation fluide; Plasma; Instabilités; Dérive ExB; Transport anormal; Propulseur de Hall; Fluid modeling; Plasma; Instabilities; ExB drift; Anomalous transport; Hall thruster

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APA (6th Edition):

Sadouni, S. (2020). Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources. (Doctoral Dissertation). Université Toulouse III – Paul Sabatier. Retrieved from http://www.theses.fr/2020TOU30014

Chicago Manual of Style (16th Edition):

Sadouni, Sarah. “Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources.” 2020. Doctoral Dissertation, Université Toulouse III – Paul Sabatier. Accessed March 07, 2021. http://www.theses.fr/2020TOU30014.

MLA Handbook (7th Edition):

Sadouni, Sarah. “Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources.” 2020. Web. 07 Mar 2021.

Vancouver:

Sadouni S. Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources. [Internet] [Doctoral dissertation]. Université Toulouse III – Paul Sabatier; 2020. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2020TOU30014.

Council of Science Editors:

Sadouni S. Modélisation fluide du transport et des instabilités dans des sources plasma froid magnétisé : Fluid modeling of transport and instabilities in magnetized low-temperature plasma sources. [Doctoral Dissertation]. Université Toulouse III – Paul Sabatier; 2020. Available from: http://www.theses.fr/2020TOU30014

23. Croes, Vivien. Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall.

Degree: Docteur es, Physique des plasmas, 2017, Université Paris-Saclay (ComUE)

Alors que les applications spatiales prennent une place de plus en plus cruciale dans nos vies, les coûts d'opération des satellites doivent être réduits. Ceci… (more)

Subjects/Keywords: Propulseur; Courant de Hall; Modélisation PIC; Astronautique; Code collisionnel; Parallèlisation massive; Thruster; Hall current; PIC modelization; Astronautics; Collisional code; Massive Parallelization

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APA (6th Edition):

Croes, V. (2017). Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall. (Doctoral Dissertation). Université Paris-Saclay (ComUE). Retrieved from http://www.theses.fr/2017SACLX060

Chicago Manual of Style (16th Edition):

Croes, Vivien. “Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall.” 2017. Doctoral Dissertation, Université Paris-Saclay (ComUE). Accessed March 07, 2021. http://www.theses.fr/2017SACLX060.

MLA Handbook (7th Edition):

Croes, Vivien. “Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall.” 2017. Web. 07 Mar 2021.

Vancouver:

Croes V. Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall. [Internet] [Doctoral dissertation]. Université Paris-Saclay (ComUE); 2017. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2017SACLX060.

Council of Science Editors:

Croes V. Plasma discharge 2D modeling of a Hall thruster : Modélisation bidimensionnelle de la décharge plasma dans un propulseur de Hall. [Doctoral Dissertation]. Université Paris-Saclay (ComUE); 2017. Available from: http://www.theses.fr/2017SACLX060


INP Toulouse

24. Rossi, Alberto. Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits.

Degree: Docteur es, Génie Électrique, 2017, INP Toulouse

 Aujourd’hui les propulseurs à effet Hall ont gagné une position dominante dans le marché des propulseurs électriques spatiales. Ce grand succès est du surtout à… (more)

Subjects/Keywords: Optimisation; Propulseur effet Hall; Circuit Magnétique; Physique des plasmas; Optimization; Magnetic Circuit; Hall effetc thruster; Plasma physics

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APA (6th Edition):

Rossi, A. (2017). Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2017INPT0035

Chicago Manual of Style (16th Edition):

Rossi, Alberto. “Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits.” 2017. Doctoral Dissertation, INP Toulouse. Accessed March 07, 2021. http://www.theses.fr/2017INPT0035.

MLA Handbook (7th Edition):

Rossi, Alberto. “Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits.” 2017. Web. 07 Mar 2021.

Vancouver:

Rossi A. Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits. [Internet] [Doctoral dissertation]. INP Toulouse; 2017. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2017INPT0035.

Council of Science Editors:

Rossi A. Développement d'outils d'optimisation dédiés aux circuits magnétiques des propulseurs à effet Hall : Optimization tools dedicated to Hall effect thrusters magnetic circuits. [Doctoral Dissertation]. INP Toulouse; 2017. Available from: http://www.theses.fr/2017INPT0035


University of Michigan

25. Choi, Yongjun. Modeling an Anode Layer Hall Thruster and its Plume.

Degree: PhD, Aerospace Engineering, 2008, University of Michigan

 A study of the D55 Hall thruster are performed. The first part of this thesis investigates the xenon plasma properties within the D55 Hall thruster(more)

Subjects/Keywords: Electric Propulsion; Hall Thruster; TAL; Thruster Channel; Aerospace Engineering; Engineering

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APA (6th Edition):

Choi, Y. (2008). Modeling an Anode Layer Hall Thruster and its Plume. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/60648

Chicago Manual of Style (16th Edition):

Choi, Yongjun. “Modeling an Anode Layer Hall Thruster and its Plume.” 2008. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/60648.

MLA Handbook (7th Edition):

Choi, Yongjun. “Modeling an Anode Layer Hall Thruster and its Plume.” 2008. Web. 07 Mar 2021.

Vancouver:

Choi Y. Modeling an Anode Layer Hall Thruster and its Plume. [Internet] [Doctoral dissertation]. University of Michigan; 2008. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/60648.

Council of Science Editors:

Choi Y. Modeling an Anode Layer Hall Thruster and its Plume. [Doctoral Dissertation]. University of Michigan; 2008. Available from: http://hdl.handle.net/2027.42/60648


University of Michigan

26. Walker, Mitchell Louis Ronald. Effects of facility backpressure on the performance and plume of a Hall thruster.

Degree: PhD, Applied Sciences, 2005, University of Michigan

 This dissertation presents research aimed at understanding the relationship between facility background pressure, Hall thruster performance, and plume characteristics. Due to the wide range of… (more)

Subjects/Keywords: Backpressure; Effects; Facility; Hall Thruster; Performance; Plume

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APA (6th Edition):

Walker, M. L. R. (2005). Effects of facility backpressure on the performance and plume of a Hall thruster. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/124969

Chicago Manual of Style (16th Edition):

Walker, Mitchell Louis Ronald. “Effects of facility backpressure on the performance and plume of a Hall thruster.” 2005. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/124969.

MLA Handbook (7th Edition):

Walker, Mitchell Louis Ronald. “Effects of facility backpressure on the performance and plume of a Hall thruster.” 2005. Web. 07 Mar 2021.

Vancouver:

Walker MLR. Effects of facility backpressure on the performance and plume of a Hall thruster. [Internet] [Doctoral dissertation]. University of Michigan; 2005. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/124969.

Council of Science Editors:

Walker MLR. Effects of facility backpressure on the performance and plume of a Hall thruster. [Doctoral Dissertation]. University of Michigan; 2005. Available from: http://hdl.handle.net/2027.42/124969


Texas A&M University

27. Mansour, Adnan. Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters.

Degree: MS, Aerospace Engineering, 2019, Texas A&M University

 The growth of plasma applications in industrial and scientific settings has led to the need for consistent computational plasma models. The multi-scale, highly nonlinear physics… (more)

Subjects/Keywords: Plasma modelling; ablating arc discharge; carbon nanomaterial synthesis; Hall-effect thruster; plasma propulsion; low temperature plasma

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APA (6th Edition):

Mansour, A. (2019). Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188773

Chicago Manual of Style (16th Edition):

Mansour, Adnan. “Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters.” 2019. Masters Thesis, Texas A&M University. Accessed March 07, 2021. http://hdl.handle.net/1969.1/188773.

MLA Handbook (7th Edition):

Mansour, Adnan. “Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters.” 2019. Web. 07 Mar 2021.

Vancouver:

Mansour A. Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters. [Internet] [Masters thesis]. Texas A&M University; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1969.1/188773.

Council of Science Editors:

Mansour A. Low Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrusters. [Masters Thesis]. Texas A&M University; 2019. Available from: http://hdl.handle.net/1969.1/188773


University of Michigan

28. Raisanen, Astrid. A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 The goal of this dissertation is to improve the state-of-the art modeling approaches available for simulating the discharge plasma in a Hall effect thruster (HET).… (more)

Subjects/Keywords: electric propulsion; Hall thruster; plasma physics; particle-in-cell (PIC); direct kinetic (DK); numerical simulation; Aerospace Engineering; Physics; Engineering; Science

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APA (6th Edition):

Raisanen, A. (2020). A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/162983

Chicago Manual of Style (16th Edition):

Raisanen, Astrid. “A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster.” 2020. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/162983.

MLA Handbook (7th Edition):

Raisanen, Astrid. “A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster.” 2020. Web. 07 Mar 2021.

Vancouver:

Raisanen A. A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/162983.

Council of Science Editors:

Raisanen A. A Two-dimensional Hybrid-Direct Kinetic Model of a Hall Thruster. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/162983

29. Grimaud, Lou. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.

Degree: Docteur es, Physique, 2018, Université d'Orléans

Les propulseurs de Hall sont l’une des techniques de propulsion fusée par plasma les plus utilisés. Ils possèdent une impulsion spécifique moyenne et un haut… (more)

Subjects/Keywords: Propulsion spatiale electrique; Propulsion par plasma; Propulseur de Hall; Écrantage magnétique; Electric space propulsion; Plasma propulsion; Hall thruster; Magnetic shielding; Laser induced fluorescence; Alternative materials; Low power; 621.46

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APA (6th Edition):

Grimaud, L. (2018). Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. (Doctoral Dissertation). Université d'Orléans. Retrieved from http://www.theses.fr/2018ORLE2046

Chicago Manual of Style (16th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Doctoral Dissertation, Université d'Orléans. Accessed March 07, 2021. http://www.theses.fr/2018ORLE2046.

MLA Handbook (7th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Web. 07 Mar 2021.

Vancouver:

Grimaud L. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. [Internet] [Doctoral dissertation]. Université d'Orléans; 2018. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2018ORLE2046.

Council of Science Editors:

Grimaud L. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. [Doctoral Dissertation]. Université d'Orléans; 2018. Available from: http://www.theses.fr/2018ORLE2046

30. Sekerak, Michael J. Plasma Oscillations and Operational Modes in Hall Effect Thrusters.

Degree: PhD, Aerospace Engineering, 2014, University of Michigan

 Mode transitions have been commonly observed in Hall effect thruster (HET) operation where a small change in a thruster operating parameter such as discharge voltage,… (more)

Subjects/Keywords: Hall Thruster; Hall Effect Thruster; Electric Propulsion; Plasma Oscillations; Mode Transitions; Aerospace Engineering; Engineering

…Busek Hall Thruster BPT Busek Primex Thruster CCW Counter Clockwise CFD Computational Fluid… …Longmier Mode transitions have been commonly observed in Hall effect thruster (HET)… …studied Hall thruster breathing mode, which is supported by time-resolved simulations of the… …Problem Statement Hall Effect Thruster (HET)s have been under development since the… …3.2.3 Thrust Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3 H6 Thruster… 

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APA (6th Edition):

Sekerak, M. J. (2014). Plasma Oscillations and Operational Modes in Hall Effect Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/107178

Chicago Manual of Style (16th Edition):

Sekerak, Michael J. “Plasma Oscillations and Operational Modes in Hall Effect Thrusters.” 2014. Doctoral Dissertation, University of Michigan. Accessed March 07, 2021. http://hdl.handle.net/2027.42/107178.

MLA Handbook (7th Edition):

Sekerak, Michael J. “Plasma Oscillations and Operational Modes in Hall Effect Thrusters.” 2014. Web. 07 Mar 2021.

Vancouver:

Sekerak MJ. Plasma Oscillations and Operational Modes in Hall Effect Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2027.42/107178.

Council of Science Editors:

Sekerak MJ. Plasma Oscillations and Operational Modes in Hall Effect Thrusters. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/107178

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