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You searched for subject:(Thruster). Showing records 1 – 30 of 131 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 September 16, 2019. 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. 16 Sep 2019.

Vancouver:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2019 Sep 16]. 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 Sydney

2. Bathgate, Stephen Norman. The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion .

Degree: 2017, University of Sydney

 The aim of the work reported in this thesis has been to explore arrangements of magnetic fields and electric currents to create novel plasma thrusters… (more)

Subjects/Keywords: magnetic reconnection; HiPIMS; plasma thruster

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APA (6th Edition):

Bathgate, S. N. (2017). The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/17025

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):

Bathgate, Stephen Norman. “The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion .” 2017. Thesis, University of Sydney. Accessed September 16, 2019. http://hdl.handle.net/2123/17025.

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

MLA Handbook (7th Edition):

Bathgate, Stephen Norman. “The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion .” 2017. Web. 16 Sep 2019.

Vancouver:

Bathgate SN. The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion . [Internet] [Thesis]. University of Sydney; 2017. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/2123/17025.

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

Council of Science Editors:

Bathgate SN. The use of magnetic fields to create high-speed plasma jets for spacecraft propulsion . [Thesis]. University of Sydney; 2017. Available from: http://hdl.handle.net/2123/17025

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


University of Victoria

3. Buchanan, M. Amos. Characterization and Control of a Saab Seaeye Thruster.

Degree: Department of Mechanical Engineering, 2015, University of Victoria

 The use of Remotely Operated Vehicles (ROVs) in exploring and building infrastructure in the ocean is expanding. ROVs are performing tasks underwater that would be… (more)

Subjects/Keywords: Thruster Control; Ocean; Remote Underwater Vehicle; ROV; Underwater Thruster; Guidance

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APA (6th Edition):

Buchanan, M. A. (2015). Characterization and Control of a Saab Seaeye Thruster. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/6003

Chicago Manual of Style (16th Edition):

Buchanan, M Amos. “Characterization and Control of a Saab Seaeye Thruster.” 2015. Masters Thesis, University of Victoria. Accessed September 16, 2019. http://hdl.handle.net/1828/6003.

MLA Handbook (7th Edition):

Buchanan, M Amos. “Characterization and Control of a Saab Seaeye Thruster.” 2015. Web. 16 Sep 2019.

Vancouver:

Buchanan MA. Characterization and Control of a Saab Seaeye Thruster. [Internet] [Masters thesis]. University of Victoria; 2015. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/1828/6003.

Council of Science Editors:

Buchanan MA. Characterization and Control of a Saab Seaeye Thruster. [Masters Thesis]. University of Victoria; 2015. Available from: http://hdl.handle.net/1828/6003


Universidade de Brasília

4. 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 September 16, 2019. 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. 16 Sep 2019.

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 2019 Sep 16]. 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


Penn State University

5. Capalungan, Erica E. Design And Development of a 30-GHz Microwave Electrothermal Thruster.

Degree: MS, Aerospace Engineering, 2011, Penn State University

 Research has been conducted on the microwave electrothermal thruster at The Pennsylvania State University since the 1980’s. Each subsequent thruster incorporated modifications that resulted in… (more)

Subjects/Keywords: Microwave Electrothermal Thruster; MET; electric propulsion

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Capalungan, E. E. (2011). Design And Development of a 30-GHz Microwave Electrothermal Thruster. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/12292

Chicago Manual of Style (16th Edition):

Capalungan, Erica E. “Design And Development of a 30-GHz Microwave Electrothermal Thruster.” 2011. Masters Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/12292.

MLA Handbook (7th Edition):

Capalungan, Erica E. “Design And Development of a 30-GHz Microwave Electrothermal Thruster.” 2011. Web. 16 Sep 2019.

Vancouver:

Capalungan EE. Design And Development of a 30-GHz Microwave Electrothermal Thruster. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/12292.

Council of Science Editors:

Capalungan EE. Design And Development of a 30-GHz Microwave Electrothermal Thruster. [Masters Thesis]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/12292


Penn State University

6. Abaimov, Mikhail D. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.

Degree: MS, Aerospace Engineering, 2015, Penn State University

 CubeSats are small satellites that conform to combinations of a standard 10×10×10 cm form factor. Currently, CubeSats have limited propulsion options because their restrictive size.… (more)

Subjects/Keywords: microwave; electrothermal; thruster; CubeSat; small; spacecraft

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APA (6th Edition):

Abaimov, M. D. (2015). Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26633

Chicago Manual of Style (16th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Masters Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/26633.

MLA Handbook (7th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Web. 16 Sep 2019.

Vancouver:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Internet] [Masters thesis]. Penn State University; 2015. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/26633.

Council of Science Editors:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Masters Thesis]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26633


Penn State University

7. Mistoco, Valerie Fabienne. MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS.

Degree: PhD, Electrical Engineering, 2011, Penn State University

 This work is motivated by the increasing interest in small-scale radio-frequency ion thrusters for micro- and nanosatellite applications, in particular for station- keeping. This specific… (more)

Subjects/Keywords: inductive discharge; plasma; ion thruster; propulsion systems

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APA (6th Edition):

Mistoco, V. F. (2011). MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9363

Chicago Manual of Style (16th Edition):

Mistoco, Valerie Fabienne. “MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS.” 2011. Doctoral Dissertation, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/9363.

MLA Handbook (7th Edition):

Mistoco, Valerie Fabienne. “MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS.” 2011. Web. 16 Sep 2019.

Vancouver:

Mistoco VF. MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS. [Internet] [Doctoral dissertation]. Penn State University; 2011. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/9363.

Council of Science Editors:

Mistoco VF. MODELING OF SMALL SCALE RADIO-FREQUENCY INDUCTIVE DISCHARGES FOR ELECTRIC PROPULSION APPLICATIONS. [Doctoral Dissertation]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/9363


University of Sydney

8. Ho, Derrick. Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV .

Degree: 2016, University of Sydney

 This thesis presents investigations on the potential lift augmentation of a Tip Thruster for driving a rotating wing (lifting surface) in a monocopter configuration, to… (more)

Subjects/Keywords: UAV; Monocopter; Aircraft; Rotary; Tip thruster; VTOL

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APA (6th Edition):

Ho, D. (2016). Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/16593

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):

Ho, Derrick. “Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV .” 2016. Thesis, University of Sydney. Accessed September 16, 2019. http://hdl.handle.net/2123/16593.

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

MLA Handbook (7th Edition):

Ho, Derrick. “Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV .” 2016. Web. 16 Sep 2019.

Vancouver:

Ho D. Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV . [Internet] [Thesis]. University of Sydney; 2016. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/2123/16593.

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

Council of Science Editors:

Ho D. Augmented Lift by Tip Thruster of an Asymmetric Single Blade Rotary Wing UAV . [Thesis]. University of Sydney; 2016. Available from: http://hdl.handle.net/2123/16593

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


Rice University

9. Kirmizi, Mehmet. Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots.

Degree: MS, Engineering, 2015, Rice University

 Nowadays, underwater robots play a significant role in many aspects of industry such as mine hunting, sea floor mapping, sub-sea pipeline construction and pipe surveys.… (more)

Subjects/Keywords: In-line Pump; Thruster; Ducted thrusters

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APA (6th Edition):

Kirmizi, M. (2015). Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/88074

Chicago Manual of Style (16th Edition):

Kirmizi, Mehmet. “Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots.” 2015. Masters Thesis, Rice University. Accessed September 16, 2019. http://hdl.handle.net/1911/88074.

MLA Handbook (7th Edition):

Kirmizi, Mehmet. “Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots.” 2015. Web. 16 Sep 2019.

Vancouver:

Kirmizi M. Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots. [Internet] [Masters thesis]. Rice University; 2015. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/1911/88074.

Council of Science Editors:

Kirmizi M. Modeling and Analysis of an In-line Pump Jet Thruster for Swimming Robots. [Masters Thesis]. Rice University; 2015. Available from: http://hdl.handle.net/1911/88074


University of Michigan

10. 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 September 16, 2019. 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. 16 Sep 2019.

Vancouver:

Huismann TD. Improving Hall Thruster Plume Simulation through Refined Characterization of Near-field Plasma Properties. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Sep 16]. 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


University of Toronto

11. 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 September 16, 2019. 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. 16 Sep 2019.

Vancouver:

Pigeon C. Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2019 Sep 16]. 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


San Jose State University

12. Kolesar, Michael David. A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser.

Degree: MS, Aerospace Engineering, 2015, San Jose State University

  With an increased interest by universities, government and commercial groups in using constellations of pico and and nano satellites, the need for micro-thrusters to… (more)

Subjects/Keywords: ablation; Laser; polymer; polyoxymethelyne; propulsion; thruster

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APA (6th Edition):

Kolesar, M. D. (2015). A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.7mea-n99e ; https://scholarworks.sjsu.edu/etd_theses/4644

Chicago Manual of Style (16th Edition):

Kolesar, Michael David. “A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser.” 2015. Masters Thesis, San Jose State University. Accessed September 16, 2019. https://doi.org/10.31979/etd.7mea-n99e ; https://scholarworks.sjsu.edu/etd_theses/4644.

MLA Handbook (7th Edition):

Kolesar, Michael David. “A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser.” 2015. Web. 16 Sep 2019.

Vancouver:

Kolesar MD. A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser. [Internet] [Masters thesis]. San Jose State University; 2015. [cited 2019 Sep 16]. Available from: https://doi.org/10.31979/etd.7mea-n99e ; https://scholarworks.sjsu.edu/etd_theses/4644.

Council of Science Editors:

Kolesar MD. A Study of Laser Ablation Propulsion Using Polyoxymethelyne and a High Power Diode Laser. [Masters Thesis]. San Jose State University; 2015. Available from: https://doi.org/10.31979/etd.7mea-n99e ; https://scholarworks.sjsu.edu/etd_theses/4644


California State University – Sacramento

13. McKown, Alissa Jane. Influence of microstructure on microwave reflectivity in copper.

Degree: MS, Mechanical Engineering, 2019, California State University – Sacramento

 To better understand the phenomena of various thrust outputs with constant energy input in the RF Resonant Cavity Thruster, a theoretical space travel propulsion system,… (more)

Subjects/Keywords: Copper; Reflectivity; Microwaves; EmDrive; RF resonant cavity thruster; Radio frequency resonant cavity thruster

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APA (6th Edition):

McKown, A. J. (2019). Influence of microstructure on microwave reflectivity in copper. (Masters Thesis). California State University – Sacramento. Retrieved from http://hdl.handle.net/10211.3/207767

Chicago Manual of Style (16th Edition):

McKown, Alissa Jane. “Influence of microstructure on microwave reflectivity in copper.” 2019. Masters Thesis, California State University – Sacramento. Accessed September 16, 2019. http://hdl.handle.net/10211.3/207767.

MLA Handbook (7th Edition):

McKown, Alissa Jane. “Influence of microstructure on microwave reflectivity in copper.” 2019. Web. 16 Sep 2019.

Vancouver:

McKown AJ. Influence of microstructure on microwave reflectivity in copper. [Internet] [Masters thesis]. California State University – Sacramento; 2019. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/10211.3/207767.

Council of Science Editors:

McKown AJ. Influence of microstructure on microwave reflectivity in copper. [Masters Thesis]. California State University – Sacramento; 2019. Available from: http://hdl.handle.net/10211.3/207767


Michigan Technological University

14. 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 September 16, 2019. https://digitalcommons.mtu.edu/etdr/690.

MLA Handbook (7th Edition):

Vanheusden, Elizabeth M. “Thermomagnetic Convective Cooling of Hall Effect Thruster.” 2018. Web. 16 Sep 2019.

Vancouver:

Vanheusden EM. Thermomagnetic Convective Cooling of Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2018. [cited 2019 Sep 16]. 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


Penn State University

15. Hsieh, Sang. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.

Degree: 2018, Penn State University

 This thesis presents an assessment of grid life for the Miniature Microwave-Frequency Ion Thruster (MMIT), which is being developed at The Pennsylvania State University. The… (more)

Subjects/Keywords: Space Propulsion; Electric Propulsion; Rocket Propulsion; Plasma Propulsion; Ion Thruster; Microwave Thruster; CubeSats; Life Assessment; Grid Erosion

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APA (6th Edition):

Hsieh, S. (2018). LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/15676suh301

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):

Hsieh, Sang. “LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/15676suh301.

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

MLA Handbook (7th Edition):

Hsieh, Sang. “LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Web. 16 Sep 2019.

Vancouver:

Hsieh S. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/15676suh301.

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

Council of Science Editors:

Hsieh S. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Thesis]. Penn State University; 2018. Available from: https://etda.libraries.psu.edu/catalog/15676suh301

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

16. Adusumilli, Rohit Prasad. PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER.

Degree: MS, Aerospace Engineering, 2011, Penn State University

 This work discusses the design and testing of a high power 14.5-GHz Miniature Microwave Electrothermal Thruster (MET) currently under development at The Pennsylvania State University.… (more)

Subjects/Keywords: Microwave Electrothermal Thruster

…Electrothermal Thruster (MET) for the past two decades. An MET uses microwave energy to… …electrostatic, electromagnetic, and electrothermal. In an electrostatic thruster, the propellant is… …thruster, colloid thruster, and Hall thruster.2 Electromagnetic thrusters use an electric field… …1000 s and 10,000 s. Some 6 examples of an electromagnetic thruster include the… …magnetoplasmadynamic thruster, pulsed plasma thruster, and pulsed inductive thruster.2 Electrothermal… 

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APA (6th Edition):

Adusumilli, R. P. (2011). PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/11876

Chicago Manual of Style (16th Edition):

Adusumilli, Rohit Prasad. “PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER.” 2011. Masters Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/11876.

MLA Handbook (7th Edition):

Adusumilli, Rohit Prasad. “PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER.” 2011. Web. 16 Sep 2019.

Vancouver:

Adusumilli RP. PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/11876.

Council of Science Editors:

Adusumilli RP. PERFORMANCE EVALUATION AND OPTIMIZATION OF HIGH POWER 14.5-GHz MINIATURE MICROWAVE ELECTROTHERMAL THRUSTER. [Masters Thesis]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/11876


Penn State University

17. Kodanganallur Narayanan, Ramachandran. Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation.

Degree: MS, Computer Science and Engineering, 2016, Penn State University

 The particle-in-cell (PIC) numerical technique is frequently used in physics and engineering simulations. In this work, we describe ES-PICBench, a new shared-memory parallel implementation of… (more)

Subjects/Keywords: electrospray; multigrid; parallel; particle-in-cell; colloid thruster

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APA (6th Edition):

Kodanganallur Narayanan, R. (2016). Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/28933

Chicago Manual of Style (16th Edition):

Kodanganallur Narayanan, Ramachandran. “Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation.” 2016. Masters Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/28933.

MLA Handbook (7th Edition):

Kodanganallur Narayanan, Ramachandran. “Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation.” 2016. Web. 16 Sep 2019.

Vancouver:

Kodanganallur Narayanan R. Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/28933.

Council of Science Editors:

Kodanganallur Narayanan R. Parallel Particle-in-cell Performance Optimization: A Case Study of Electrospray Simulation. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/28933


Penn State University

18. Blum, Jacob. PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.

Degree: MS, Aerospace Engineering, 2009, Penn State University

 The performance of an 8-GHz microwave electrothermal thruster was measured using various thrust stand configurations with nitrogen gas as the propellant. The momentum of the… (more)

Subjects/Keywords: MET; microwave electrothermal thruster; electric propulsion; aerospace engineering

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APA (6th Edition):

Blum, J. (2009). PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9608

Chicago Manual of Style (16th Edition):

Blum, Jacob. “PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.” 2009. Masters Thesis, Penn State University. Accessed September 16, 2019. https://etda.libraries.psu.edu/catalog/9608.

MLA Handbook (7th Edition):

Blum, Jacob. “PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.” 2009. Web. 16 Sep 2019.

Vancouver:

Blum J. PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Sep 16]. Available from: https://etda.libraries.psu.edu/catalog/9608.

Council of Science Editors:

Blum J. PERFORMANCE EVALUATION AND OPTIMIZATION OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9608

19. Aheieva, Kateryna. Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発.

Degree: 博士(工学), 2017, Kyushu Institute of Technology / 九州工業大学

九州工業大学博士学位論文 学位記番号:工博甲第422号 学位授与年月日:平成28年9月23日

1. Introduction|2. Experimental apparatus and test setup|3. Vacuum Arc Thruster|4. Satellite deorbit system based on the Vacuum Arc Thruster|5. Vacuum Arc Thruster on-board satellite Horyu-4|6. Conclusions

平成28年度

Advisors/Committee Members: 豊田, 和弘.

Subjects/Keywords: Electric propulsion; Nanosatellites; Plasma; Space debris; deorbiting; Vacuum arc thruster

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APA (6th Edition):

Aheieva, K. (2017). Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発. (Thesis). Kyushu Institute of Technology / 九州工業大学. Retrieved from http://hdl.handle.net/10228/5971

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):

Aheieva, Kateryna. “Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発.” 2017. Thesis, Kyushu Institute of Technology / 九州工業大学. Accessed September 16, 2019. http://hdl.handle.net/10228/5971.

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

MLA Handbook (7th Edition):

Aheieva, Kateryna. “Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発.” 2017. Web. 16 Sep 2019.

Vancouver:

Aheieva K. Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発. [Internet] [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/10228/5971.

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

Council of Science Editors:

Aheieva K. Development of a Vacuum Arc Thruster for Nanosatellites : 超小型衛星搭載用真空アーク推進機の開発. [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. Available from: http://hdl.handle.net/10228/5971

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


University of Southern California

20. Schilling, John. Development of the two-stage micro pulsed plasma thruster.

Degree: PhD, Astronautical Engineering, 2007, University of Southern California

 In this dissertation, the development of the two-stage micro pulsed plasma thruster (uPPT) is described. This development followed from a research effort aimed at overcoming… (more)

Subjects/Keywords: micro PPT; pulsed plasma thruster

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APA (6th Edition):

Schilling, J. (2007). Development of the two-stage micro pulsed plasma thruster. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/162270/rec/1968

Chicago Manual of Style (16th Edition):

Schilling, John. “Development of the two-stage micro pulsed plasma thruster.” 2007. Doctoral Dissertation, University of Southern California. Accessed September 16, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/162270/rec/1968.

MLA Handbook (7th Edition):

Schilling, John. “Development of the two-stage micro pulsed plasma thruster.” 2007. Web. 16 Sep 2019.

Vancouver:

Schilling J. Development of the two-stage micro pulsed plasma thruster. [Internet] [Doctoral dissertation]. University of Southern California; 2007. [cited 2019 Sep 16]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/162270/rec/1968.

Council of Science Editors:

Schilling J. Development of the two-stage micro pulsed plasma thruster. [Doctoral Dissertation]. University of Southern California; 2007. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/162270/rec/1968


University of Saskatchewan

21. 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 September 16, 2019. 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. 16 Sep 2019.

Vancouver:

Morin V1. Sheath Boundary Effects on the Stability of Hall Plasmas. [Internet] [Thesis]. University of Saskatchewan; 2018. [cited 2019 Sep 16]. 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

22. Weber, Thomas. The Electrodeless Lorentz Force Thruster Experiment.

Degree: 2010, University of Washington

 The Electrodeless Lorentz Force (ELF) thruster is a novel type of plasma thruster, which utilizes Rotating Magnetic Field current drive within a diverging magnetic field… (more)

Subjects/Keywords: thruster; plasma; FRC; RMF

…along the axis of the thruster. 131 3.30 Internal B-probe oriented to measure the axial field… …within the thruster.132 3.31 Density profile within the thruster… …introduction to the Electrodeless Lorentz Force (ELF) thruster experimental program… …Motivation for the development of an ELF-type thruster precedes a brief review of the physical… …processes taking place within the ELF thruster, including the utility of Field Reversed… 

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APA (6th Edition):

Weber, T. (2010). The Electrodeless Lorentz Force Thruster Experiment. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/20069

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):

Weber, Thomas. “The Electrodeless Lorentz Force Thruster Experiment.” 2010. Thesis, University of Washington. Accessed September 16, 2019. http://hdl.handle.net/1773/20069.

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

MLA Handbook (7th Edition):

Weber, Thomas. “The Electrodeless Lorentz Force Thruster Experiment.” 2010. Web. 16 Sep 2019.

Vancouver:

Weber T. The Electrodeless Lorentz Force Thruster Experiment. [Internet] [Thesis]. University of Washington; 2010. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/1773/20069.

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

Council of Science Editors:

Weber T. The Electrodeless Lorentz Force Thruster Experiment. [Thesis]. University of Washington; 2010. Available from: http://hdl.handle.net/1773/20069

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


Princeton University

23. Hallock, Ashley Kristin. Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator .

Degree: PhD, 2012, Princeton University

 The effect of inductive coil geometry on the operating characteristics of a pulsed inductive plasma thruster is investigated analytically and experimentally. Coil inductance is measured… (more)

Subjects/Keywords: Conical; Electric Propulsion; Geometry; Plasma; Pulsed Inductive; Thruster

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APA (6th Edition):

Hallock, A. K. (2012). Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator . (Doctoral Dissertation). Princeton University. Retrieved from http://arks.princeton.edu/ark:/88435/dsp017w62f8256

Chicago Manual of Style (16th Edition):

Hallock, Ashley Kristin. “Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator .” 2012. Doctoral Dissertation, Princeton University. Accessed September 16, 2019. http://arks.princeton.edu/ark:/88435/dsp017w62f8256.

MLA Handbook (7th Edition):

Hallock, Ashley Kristin. “Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator .” 2012. Web. 16 Sep 2019.

Vancouver:

Hallock AK. Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator . [Internet] [Doctoral dissertation]. Princeton University; 2012. [cited 2019 Sep 16]. Available from: http://arks.princeton.edu/ark:/88435/dsp017w62f8256.

Council of Science Editors:

Hallock AK. Effect of Inductive Coil Geometry on the Operating Characteristics of a Pulsed Inductive Plasma Accelerator . [Doctoral Dissertation]. Princeton University; 2012. Available from: http://arks.princeton.edu/ark:/88435/dsp017w62f8256


Mississippi State University

24. Reneau, Jarred. INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL.

Degree: MS, Aerospace Engineering, 2011, Mississippi State University

  Electric propulsion systems utilize electrical energy to produce thrust for spacecraft propulsion. These systems have multiple applications ranging from Earth orbit North-South station keeping… (more)

Subjects/Keywords: electormagnetic propulsion; electromagnetic; Pulsed Inductive Thruster; NASA; Electric propulsion; energy equation

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APA (6th Edition):

Reneau, J. (2011). INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-04012011-141046/ ;

Chicago Manual of Style (16th Edition):

Reneau, Jarred. “INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL.” 2011. Masters Thesis, Mississippi State University. Accessed September 16, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04012011-141046/ ;.

MLA Handbook (7th Edition):

Reneau, Jarred. “INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL.” 2011. Web. 16 Sep 2019.

Vancouver:

Reneau J. INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL. [Internet] [Masters thesis]. Mississippi State University; 2011. [cited 2019 Sep 16]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04012011-141046/ ;.

Council of Science Editors:

Reneau J. INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL. [Masters Thesis]. Mississippi State University; 2011. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04012011-141046/ ;

25. Gerst, Jan Dennis. Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale.

Degree: Docteur es, Physique, 2013, Université d'Orléans

Le propulseur PEGASES (Plasma Propulsion with Electronegative Gases) est un nouveau type de propulseur électrique pour la propulsion spatiale. Il utilise des ions négatifs et… (more)

Subjects/Keywords: Plasma; Propulsion électrique; Propulseur ionique; Plasma; Electric propulsion; Ion thruster

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APA (6th Edition):

Gerst, J. D. (2013). Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale. (Doctoral Dissertation). Université d'Orléans. Retrieved from http://www.theses.fr/2013ORLE2036

Chicago Manual of Style (16th Edition):

Gerst, Jan Dennis. “Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale.” 2013. Doctoral Dissertation, Université d'Orléans. Accessed September 16, 2019. http://www.theses.fr/2013ORLE2036.

MLA Handbook (7th Edition):

Gerst, Jan Dennis. “Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale.” 2013. Web. 16 Sep 2019.

Vancouver:

Gerst JD. Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale. [Internet] [Doctoral dissertation]. Université d'Orléans; 2013. [cited 2019 Sep 16]. Available from: http://www.theses.fr/2013ORLE2036.

Council of Science Editors:

Gerst JD. Investigation of magnetized radio frequency plasma sources for electric space propulsion : Sources plasma RF magnétisées : applications à la propulsion spatiale. [Doctoral Dissertation]. Université d'Orléans; 2013. Available from: http://www.theses.fr/2013ORLE2036

26. de Chadenedes, Mark L. Propulsion performance of a microcavity discharge device.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

 This work explores the requirements for an effective nanosatellite propulsion system. A candidate system is proposed in the form of a microcavity discharge device modified… (more)

Subjects/Keywords: Microcavity; discharge; thruster; microcavity discharge; microcavity discharge thruster; electrothermal; electrothermal thruster; plasma; plasma thruster

…intended primary application for the MCD thruster is nanosatellites (satellites of mass < 10… …kg), such as those designed to the Cube Sat specification. The MCD thruster is… …number of EP systems have been successfully deployed including the pulsed plasma thruster… …x28;10% η, 1000 s Isp); the resistojet (50%, 300 s); the Hall thruster (50… …2000 s); and the ion thruster (70%, 3000 s). Other EP systems in advanced… 

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APA (6th Edition):

de Chadenedes, M. L. (2011). Propulsion performance of a microcavity discharge device. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/24167

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):

de Chadenedes, Mark L. “Propulsion performance of a microcavity discharge device.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed September 16, 2019. http://hdl.handle.net/2142/24167.

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

MLA Handbook (7th Edition):

de Chadenedes, Mark L. “Propulsion performance of a microcavity discharge device.” 2011. Web. 16 Sep 2019.

Vancouver:

de Chadenedes ML. Propulsion performance of a microcavity discharge device. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/2142/24167.

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

Council of Science Editors:

de Chadenedes ML. Propulsion performance of a microcavity discharge device. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/24167

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


Rice University

27. Karalomlu, Ali. Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots.

Degree: MS, Engineering, 2016, Rice University

 Throughout history, machines have replaced human labor in many industries. Our machines have made it possible to transcend human limitations. In the present day, underwater… (more)

Subjects/Keywords: In-line Pump; Centrifugal Pump; Swimming Robots; Thruster; Characterization

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APA (6th Edition):

Karalomlu, A. (2016). Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/96564

Chicago Manual of Style (16th Edition):

Karalomlu, Ali. “Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots.” 2016. Masters Thesis, Rice University. Accessed September 16, 2019. http://hdl.handle.net/1911/96564.

MLA Handbook (7th Edition):

Karalomlu, Ali. “Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots.” 2016. Web. 16 Sep 2019.

Vancouver:

Karalomlu A. Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots. [Internet] [Masters thesis]. Rice University; 2016. [cited 2019 Sep 16]. Available from: http://hdl.handle.net/1911/96564.

Council of Science Editors:

Karalomlu A. Characterization of a Submersible In-line Pump as a Thrust Generator for Swimming Robots. [Masters Thesis]. Rice University; 2016. Available from: http://hdl.handle.net/1911/96564


University of Southern California

28. Codron, Douglas A. An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges.

Degree: PhD, Astronautical Engineering, 2012, University of Southern California

 Since the early to mid 1960’s, laboratory studies have demonstrated the unique ability of magnetoplasmadynamic (MPD) thrusters to deliver an exceptionally high level of specific… (more)

Subjects/Keywords: electric propulsion; arc discharge; magntoplasmadynamic thruster; cathode; plasma; space

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APA (6th Edition):

Codron, D. A. (2012). An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/52633/rec/751

Chicago Manual of Style (16th Edition):

Codron, Douglas A. “An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges.” 2012. Doctoral Dissertation, University of Southern California. Accessed September 16, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/52633/rec/751.

MLA Handbook (7th Edition):

Codron, Douglas A. “An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges.” 2012. Web. 16 Sep 2019.

Vancouver:

Codron DA. An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges. [Internet] [Doctoral dissertation]. University of Southern California; 2012. [cited 2019 Sep 16]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/52633/rec/751.

Council of Science Editors:

Codron DA. An experimental investigation of cathode erosion in high current magnetoplasmadynamic arc discharges. [Doctoral Dissertation]. University of Southern California; 2012. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/52633/rec/751


University of Toronto

29. 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 September 16, 2019. 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. 16 Sep 2019.

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 2019 Sep 16]. 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


Arizona State University

30. Verbin, Andrew Joseph. Detailed Design of a Pulsed Plasma Thrust Stand.

Degree: Aerospace Engineering, 2017, Arizona State University

 This thesis gives a detailed design process for a pulsed type thruster. The thrust stand designed in this paper is for a Pulsed Plasma Thruster(more)

Subjects/Keywords: Aerospace engineering; Design; Engineering; Design; Plasma; Pulsed; Thrust; Thruster

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Verbin, A. J. (2017). Detailed Design of a Pulsed Plasma Thrust Stand. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/44012

Chicago Manual of Style (16th Edition):

Verbin, Andrew Joseph. “Detailed Design of a Pulsed Plasma Thrust Stand.” 2017. Masters Thesis, Arizona State University. Accessed September 16, 2019. http://repository.asu.edu/items/44012.

MLA Handbook (7th Edition):

Verbin, Andrew Joseph. “Detailed Design of a Pulsed Plasma Thrust Stand.” 2017. Web. 16 Sep 2019.

Vancouver:

Verbin AJ. Detailed Design of a Pulsed Plasma Thrust Stand. [Internet] [Masters thesis]. Arizona State University; 2017. [cited 2019 Sep 16]. Available from: http://repository.asu.edu/items/44012.

Council of Science Editors:

Verbin AJ. Detailed Design of a Pulsed Plasma Thrust Stand. [Masters Thesis]. Arizona State University; 2017. Available from: http://repository.asu.edu/items/44012

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