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You searched for +publisher:"University of Michigan" +contributor:("Gallimore, Alec D."). Showing records 1 – 30 of 48 total matches.

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1. McDonald, Michael Sean. Electron Transport in Hall Thrusters.

Degree: PhD, Applied Physics, 2012, University of Michigan

 Despite high technological maturity and a long flight heritage, computer models of Hall thrusters remain dependent on empirical inputs and a large part of thruster… (more)

Subjects/Keywords: Hall Thrusters; Electron Transport; Anomalous Transport; Cross-field Transport; Rotating Spoke Instability; High-speed Camera; Aerospace Engineering; Physics; Engineering; Science

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APA (6th Edition):

McDonald, M. S. (2012). Electron Transport in Hall Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/91553

Chicago Manual of Style (16th Edition):

McDonald, Michael Sean. “Electron Transport in Hall Thrusters.” 2012. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/91553.

MLA Handbook (7th Edition):

McDonald, Michael Sean. “Electron Transport in Hall Thrusters.” 2012. Web. 14 Dec 2019.

Vancouver:

McDonald MS. Electron Transport in Hall Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/91553.

Council of Science Editors:

McDonald MS. Electron Transport in Hall Thrusters. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/91553


University of Michigan

2. Bell, Iverson C. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.

Degree: PhD, Electrical Engineering, 2015, University of Michigan

 The work presented in this thesis evaluates the potential of electrodynamic tether (EDT) propulsion technology to provide picosatellites (100 g–1 kg) and femtosatellites (<100 g)… (more)

Subjects/Keywords: electrodynamic tether; small spacecraft; Electrical Engineering; Engineering

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APA (6th Edition):

Bell, I. C. (2015). A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/113575

Chicago Manual of Style (16th Edition):

Bell, Iverson C. “A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.” 2015. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/113575.

MLA Handbook (7th Edition):

Bell, Iverson C. “A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities.” 2015. Web. 14 Dec 2019.

Vancouver:

Bell IC. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/113575.

Council of Science Editors:

Bell IC. A System Concept Study and Experimental Evaluation of Miniaturized Electrodynamic Tethers to Enhance Picosatellite and Femtosatellite Capabilities. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/113575


University of Michigan

3. Smith, Brandon Denis. A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters.

Degree: PhD, Aerospace Engineering, 2015, University of Michigan

 This dissertation describes the development and application of numerical models for the analysis of channel wall erosion and the transport of erosion products in Hall… (more)

Subjects/Keywords: Hall thrusters; Electric propulsion; Discharge channel erosion; Atomic sputtering; Aerospace Engineering; Engineering

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APA (6th Edition):

Smith, B. D. (2015). A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/116633

Chicago Manual of Style (16th Edition):

Smith, Brandon Denis. “A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters.” 2015. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/116633.

MLA Handbook (7th Edition):

Smith, Brandon Denis. “A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters.” 2015. Web. 14 Dec 2019.

Vancouver:

Smith BD. A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/116633.

Council of Science Editors:

Smith BD. A Numerical Study of Wall Erosion and Material Transport in Hall Thrusters. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/116633


University of Michigan

4. Farbar, Erin D. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.

Degree: PhD, Aerospace Engineering, 2010, University of Michigan

 When a vehicle enters the Earth's atmosphere at the very large velocities associated with Lunar and Mars return, a strong bow shock is formed in… (more)

Subjects/Keywords: Direct Simulation Monte Carlo; Nonequilibrium Flow; Reentry Flow; Rarefied Gas Dynamics; Weakly Ionized Plasma; Hypersonic Aerothermodynamics; Aerospace Engineering; Engineering

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APA (6th Edition):

Farbar, E. D. (2010). Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/78779

Chicago Manual of Style (16th Edition):

Farbar, Erin D. “Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.” 2010. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/78779.

MLA Handbook (7th Edition):

Farbar, Erin D. “Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.” 2010. Web. 14 Dec 2019.

Vancouver:

Farbar ED. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. [Internet] [Doctoral dissertation]. University of Michigan; 2010. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/78779.

Council of Science Editors:

Farbar ED. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. [Doctoral Dissertation]. University of Michigan; 2010. Available from: http://hdl.handle.net/2027.42/78779


University of Michigan

5. Weatherford, Brandon Robert. Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2011, University of Michigan

 In electrostatic ion thrusters and Hall thrusters, electron sources are used for propellant ionization and neutralization of the thruster beam. Thermionic emitter-based sources are commonly… (more)

Subjects/Keywords: Plasma Physics; Electric Propulsion; Plasma Cathode; Electron Cyclotron Resonance; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Weatherford, B. R. (2011). Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/89714

Chicago Manual of Style (16th Edition):

Weatherford, Brandon Robert. “Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications.” 2011. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/89714.

MLA Handbook (7th Edition):

Weatherford, Brandon Robert. “Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications.” 2011. Web. 14 Dec 2019.

Vancouver:

Weatherford BR. Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/89714.

Council of Science Editors:

Weatherford BR. Development and Study of an Electron Cyclotron Resonance Waveguide Plasma Cathode for Electric Propulsion Applications. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/89714


University of Michigan

6. 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 December 14, 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. 14 Dec 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 Dec 14]. 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 Michigan

7. Lobbia, Robert Bryant. A Time-resolved Investigation of the Hall Thruster Breathing Mode.

Degree: PhD, Aerospace Engineering, 2010, University of Michigan

 The existence of plasma oscillations in the near and far field discharge of a Hall effect thruster alters the conventionally held view of their operation… (more)

Subjects/Keywords: Hall Thruster; Langmuir Probe; High-speed Measurements; Plasma; Electric Propulsion; Aerospace Engineering; Engineering

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APA (6th Edition):

Lobbia, R. B. (2010). A Time-resolved Investigation of the Hall Thruster Breathing Mode. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/76022

Chicago Manual of Style (16th Edition):

Lobbia, Robert Bryant. “A Time-resolved Investigation of the Hall Thruster Breathing Mode.” 2010. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/76022.

MLA Handbook (7th Edition):

Lobbia, Robert Bryant. “A Time-resolved Investigation of the Hall Thruster Breathing Mode.” 2010. Web. 14 Dec 2019.

Vancouver:

Lobbia RB. A Time-resolved Investigation of the Hall Thruster Breathing Mode. [Internet] [Doctoral dissertation]. University of Michigan; 2010. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/76022.

Council of Science Editors:

Lobbia RB. A Time-resolved Investigation of the Hall Thruster Breathing Mode. [Doctoral Dissertation]. University of Michigan; 2010. Available from: http://hdl.handle.net/2027.42/76022


University of Michigan

8. Dragnea, Horatiu. Development and Application of Multidimensional Computational Models for Hall Thrusters.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 The goal of this work is to aid the development of high-power Hall-effect thrusters through modeling and simulation. The focus is both on improving the… (more)

Subjects/Keywords: electric propulsion (EP); high-power Hall-effect thrusters (HET); nested channel Hall thrusters (NHT); modeling and simulation; computational plasma physics; direct Simulation Monte-Carlo (DSMC), full-fluid, hybrid-particle-in-cell (hybrid-PIC); Cartesian 2D-axisymmetric fluid electron model; Aerospace Engineering; Electrical Engineering; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Dragnea, H. (2018). Development and Application of Multidimensional Computational Models for Hall Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/147521

Chicago Manual of Style (16th Edition):

Dragnea, Horatiu. “Development and Application of Multidimensional Computational Models for Hall Thrusters.” 2018. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/147521.

MLA Handbook (7th Edition):

Dragnea, Horatiu. “Development and Application of Multidimensional Computational Models for Hall Thrusters.” 2018. Web. 14 Dec 2019.

Vancouver:

Dragnea H. Development and Application of Multidimensional Computational Models for Hall Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/147521.

Council of Science Editors:

Dragnea H. Development and Application of Multidimensional Computational Models for Hall Thrusters. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/147521


University of Michigan

9. 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 December 14, 2019. 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. 14 Dec 2019.

Vancouver:

Huang W. Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Dec 14]. 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


University of Michigan

10. Hall, Scott. Characterization of a 100-kW Class Nested-Channel Hall Thruster.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 The next generation of electric propulsion consists of systems in excess of 300 kW of power. These systems enable a wide variety of missions, including… (more)

Subjects/Keywords: electric propulsion; high power Hall thruster; Aerospace Engineering; Engineering

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APA (6th Edition):

Hall, S. (2018). Characterization of a 100-kW Class Nested-Channel Hall Thruster. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/144053

Chicago Manual of Style (16th Edition):

Hall, Scott. “Characterization of a 100-kW Class Nested-Channel Hall Thruster.” 2018. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/144053.

MLA Handbook (7th Edition):

Hall, Scott. “Characterization of a 100-kW Class Nested-Channel Hall Thruster.” 2018. Web. 14 Dec 2019.

Vancouver:

Hall S. Characterization of a 100-kW Class Nested-Channel Hall Thruster. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/144053.

Council of Science Editors:

Hall S. Characterization of a 100-kW Class Nested-Channel Hall Thruster. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/144053

11. Shabshelowitz, Adam. Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Satellites in low Earth orbit experience an aerodynamic drag force due to the finite density of gas in the thermosphere. Left unchecked, this drag force… (more)

Subjects/Keywords: Electric Propulsion; Space Propulsion; RF Plasma; Aerospace Engineering; Engineering

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APA (6th Edition):

Shabshelowitz, A. (2013). Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/98016

Chicago Manual of Style (16th Edition):

Shabshelowitz, Adam. “Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/98016.

MLA Handbook (7th Edition):

Shabshelowitz, Adam. “Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion.” 2013. Web. 14 Dec 2019.

Vancouver:

Shabshelowitz A. Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/98016.

Council of Science Editors:

Shabshelowitz A. Study of RF Plasma Technology Applied to Air-Breathing Electric Propulsion. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/98016

12. Hubble, Aimee Ann. Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2013, University of Michigan

 The objective of this dissertation is to experimentally analyze plasma transport to the anode in multicusp discharge chambers and evaluate its impact on discharge performance.… (more)

Subjects/Keywords: Magnetic Cusps; Low-temperature Plasmas; Electric Propulsion; Ion Thrusters; Nuclear Engineering and Radiological Sciences; Engineering

Page 1

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APA (6th Edition):

Hubble, A. A. (2013). Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/99970

Chicago Manual of Style (16th Edition):

Hubble, Aimee Ann. “Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/99970.

MLA Handbook (7th Edition):

Hubble, Aimee Ann. “Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources.” 2013. Web. 14 Dec 2019.

Vancouver:

Hubble AA. Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/99970.

Council of Science Editors:

Hubble AA. Experimental Assessment of Plasma Transport in Magnetic Multicusp Ion Sources. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/99970

13. Hara, Kentaro. Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas.

Degree: PhD, Aerospace Engineering, 2015, University of Michigan

 Novel computational methods were developed and used to characterize plasma flows and improve the efficiency of electric propulsion devices. The focus of this doctoral research… (more)

Subjects/Keywords: Grid-based Kinetic Plasma Simulation; Electric Propulsion; Ionization Oscillations; Aerospace Engineering; Engineering

…the University of Michigan, is shown in Fig. 1.1(a). Also illustrated are the… 

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APA (6th Edition):

Hara, K. (2015). Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/111379

Chicago Manual of Style (16th Edition):

Hara, Kentaro. “Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas.” 2015. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/111379.

MLA Handbook (7th Edition):

Hara, Kentaro. “Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas.” 2015. Web. 14 Dec 2019.

Vancouver:

Hara K. Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/111379.

Council of Science Editors:

Hara K. Development of Grid-Based Direct Kinetic Method and Hybrid Kinetic-Continuum Modeling of Hall Thruster Discharge Plasmas. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/111379

14. Giuliano, Paul Nicholas. Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 This work involves the modeling of fundamental plasma physics processes occurring within environments that are similar to that of the discharge and plume regions of… (more)

Subjects/Keywords: Electric Propulsion; Plasma Transport; Secondary Emission; Aerospace Engineering; Engineering

…Los Angeles (UCLA), as part of the University of Michigan/AFRL Center for… 

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APA (6th Edition):

Giuliano, P. N. (2013). Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/97870

Chicago Manual of Style (16th Edition):

Giuliano, Paul Nicholas. “Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/97870.

MLA Handbook (7th Edition):

Giuliano, Paul Nicholas. “Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell.” 2013. Web. 14 Dec 2019.

Vancouver:

Giuliano PN. Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/97870.

Council of Science Editors:

Giuliano PN. Modeling Fundamental Plasma Transport and Particle-Induced Emission in a Simplified Test Cell. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/97870

15. Lemmer, Kristina Marian. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.

Degree: PhD, Aerospace Engineering, 2009, University of Michigan

 During atmospheric re-entry and hypersonic flight, a bow shock forms around the vehicle leading edge. The air becomes super-heated as it passes through the shock,… (more)

Subjects/Keywords: Helicon Source; Atmospheric Re-entry; Communications Blackout; Aerospace Engineering; Engineering

…Tracking and Data Relay Satellite UM University of Michigan USAF United States Air Force… …x28;DSMC)-Computational Fluid Dynamics (CFD) code at the University of… …Michigan to simulate rarified gas flows, including simulations of non-equilibrium hypersonic… 

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APA (6th Edition):

Lemmer, K. M. (2009). Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/63673

Chicago Manual of Style (16th Edition):

Lemmer, Kristina Marian. “Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.” 2009. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/63673.

MLA Handbook (7th Edition):

Lemmer, Kristina Marian. “Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.” 2009. Web. 14 Dec 2019.

Vancouver:

Lemmer KM. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. [Internet] [Doctoral dissertation]. University of Michigan; 2009. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/63673.

Council of Science Editors:

Lemmer KM. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. [Doctoral Dissertation]. University of Michigan; 2009. Available from: http://hdl.handle.net/2027.42/63673

16. Tang, Ricky. Study of the Gasdynamic Mirror (GDM) Propulsion System.

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

 The gasdynamic mirror (GDM) is a magnetic confinement device that has been proposed as a concept which could form the basis of a spacecraft propulsion… (more)

Subjects/Keywords: Gasdynamic Mirror; GDM; Fusion Propulsion; Electrodeless; Microwave Plasma; Electron Cyclotron Resonance; Aerospace Engineering; Engineering

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APA (6th Edition):

Tang, R. (2011). Study of the Gasdynamic Mirror (GDM) Propulsion System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/86577

Chicago Manual of Style (16th Edition):

Tang, Ricky. “Study of the Gasdynamic Mirror (GDM) Propulsion System.” 2011. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/86577.

MLA Handbook (7th Edition):

Tang, Ricky. “Study of the Gasdynamic Mirror (GDM) Propulsion System.” 2011. Web. 14 Dec 2019.

Vancouver:

Tang R. Study of the Gasdynamic Mirror (GDM) Propulsion System. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/86577.

Council of Science Editors:

Tang R. Study of the Gasdynamic Mirror (GDM) Propulsion System. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/86577

17. Shastry, Rohit. Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime.

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

 Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools that can substantially reduce the need for expensive lifetime testing to… (more)

Subjects/Keywords: Electric Propulsion; Hall Thrusters; Plasma-wall Interactions; Aerospace Engineering; Engineering

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APA (6th Edition):

Shastry, R. (2011). Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/84654

Chicago Manual of Style (16th Edition):

Shastry, Rohit. “Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime.” 2011. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/84654.

MLA Handbook (7th Edition):

Shastry, Rohit. “Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime.” 2011. Web. 14 Dec 2019.

Vancouver:

Shastry R. Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/84654.

Council of Science Editors:

Shastry R. Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/84654

18. Ohlandt, Chad J. R. A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System.

Degree: PhD, Aerospace Engineering and Scientific Computing, 2011, University of Michigan

 This work advances the gasdynamic mirror (GDM) fusion space propulsion system concept by testing the potential of an advanced aneutronic fusion fuel combination of proton−11boron… (more)

Subjects/Keywords: Magnetohydrodynamic MHD; Gasdynamic Mirror GDM; Fusion Space Propulsion; Aerospace Engineering; Engineering

…containment. At the University of Michigan, significant progress has been made in… …in numerical modeling at the University of Michigan revolved around modeling complex… 

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APA (6th Edition):

Ohlandt, C. J. R. (2011). A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/86262

Chicago Manual of Style (16th Edition):

Ohlandt, Chad J R. “A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System.” 2011. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/86262.

MLA Handbook (7th Edition):

Ohlandt, Chad J R. “A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System.” 2011. Web. 14 Dec 2019.

Vancouver:

Ohlandt CJR. A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/86262.

Council of Science Editors:

Ohlandt CJR. A Computational Magnetohydrodynamic Model of a Gasdynamic Fusion Space Propulsion System. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/86262

19. Asbury, Stephen T. Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2012, University of Michigan

 Genetic Algorithms (GA) are a powerful search and optimization technique that can be applied to numerous problems. Unfortunately, GA relies on large numbers of fitness… (more)

Subjects/Keywords: Genetic Algorithm; Radiation Shield; Nuclear Engineering and Radiological Sciences; Engineering

…x28;1998)]. John Holland at the University of Michigan [Holland (1992,1975… …clusters at the University of Michigan. This model is described in Section 2.8.1. 2.3.1… 

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APA (6th Edition):

Asbury, S. T. (2012). Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/91388

Chicago Manual of Style (16th Edition):

Asbury, Stephen T. “Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design.” 2012. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/91388.

MLA Handbook (7th Edition):

Asbury, Stephen T. “Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design.” 2012. Web. 14 Dec 2019.

Vancouver:

Asbury ST. Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/91388.

Council of Science Editors:

Asbury ST. Multi-Grid Genetic Algorithms For Optimal Radiation Shield Design. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/91388

20. Mehta, Manish. Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars.

Degree: PhD, Atmospheric and Space Sciences, 2010, University of Michigan

 Pulsed supersonic jets or rocket plumes have different surface flow physics than steady jets, in particular in tenuous atmospheres such as that of Mars where… (more)

Subjects/Keywords: Supersonic Jets/Rocket Plumes/Gas Dynamics; Cratering Physics; Multiphase Fluid Dynamics; Radiometry; Mars, Water; Spacecraft, Entry, Descent and Landing; Aerospace Engineering; Atmospheric, Oceanic and Space Sciences; Physics; Engineering; Science

…Bottom) Schematic of the CFTB experimental setup at University of Michigan… …interactions [NASA JPL (Phoenix CDR), 2004]. Our group at the University of… …Michigan proposed to conduct this research into two different phases: (a) plume-surface… 

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APA (6th Edition):

Mehta, M. (2010). Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/78975

Chicago Manual of Style (16th Edition):

Mehta, Manish. “Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars.” 2010. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/78975.

MLA Handbook (7th Edition):

Mehta, Manish. “Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars.” 2010. Web. 14 Dec 2019.

Vancouver:

Mehta M. Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars. [Internet] [Doctoral dissertation]. University of Michigan; 2010. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/78975.

Council of Science Editors:

Mehta M. Plume-Surface Interactions due to Spacecraft Landings and The Discovery of Water on Mars. [Doctoral Dissertation]. University of Michigan; 2010. Available from: http://hdl.handle.net/2027.42/78975

21. Spencer, Laura Frances. The Study of CO2 Conversion in a Microwave Plasma/Catalyst System.

Degree: PhD, Applied Physics, 2012, University of Michigan

 The continual and increasing use of fossil fuels throughout the world has advanced concerns of atmospheric carbon dioxide (CO2) concentrations, causing a swell of scientific… (more)

Subjects/Keywords: Microwave Plasma; Carbon Dioxide; Energy Efficiency; Dissociation; Engineering (General); Physics; Engineering; Science

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APA (6th Edition):

Spencer, L. F. (2012). The Study of CO2 Conversion in a Microwave Plasma/Catalyst System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/94076

Chicago Manual of Style (16th Edition):

Spencer, Laura Frances. “The Study of CO2 Conversion in a Microwave Plasma/Catalyst System.” 2012. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/94076.

MLA Handbook (7th Edition):

Spencer, Laura Frances. “The Study of CO2 Conversion in a Microwave Plasma/Catalyst System.” 2012. Web. 14 Dec 2019.

Vancouver:

Spencer LF. The Study of CO2 Conversion in a Microwave Plasma/Catalyst System. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/94076.

Council of Science Editors:

Spencer LF. The Study of CO2 Conversion in a Microwave Plasma/Catalyst System. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/94076

22. Gillman, Eric D. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2012, University of Michigan

 Vehicles traveling at hypersonic velocities in the atmosphere are readily enveloped by a dense plasma layer that blocks, reflects, and significantly attenuates radio signals typically… (more)

Subjects/Keywords: Radio Blackout Mitigation; Hypersonic Vehicle Communications; Plasma Discharge; Dusty Plasma; Cathode Spot Arc; Aerospace Engineering; Nuclear Engineering and Radiological Sciences; Physics; Engineering; Science

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APA (6th Edition):

Gillman, E. D. (2012). Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/95986

Chicago Manual of Style (16th Edition):

Gillman, Eric D. “Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.” 2012. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/95986.

MLA Handbook (7th Edition):

Gillman, Eric D. “Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.” 2012. Web. 14 Dec 2019.

Vancouver:

Gillman ED. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/95986.

Council of Science Editors:

Gillman ED. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/95986

23. Arthur, Neil. Increasing the Extracted Beam Current Density in Ion Thrusters.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2017, University of Michigan

 on thrusters have seen application on space science missions and numerous satellite missions. Ion engines offer higher electrical efficiency and specific impulse capability coupled with… (more)

Subjects/Keywords: Ion Thruster; Electric Propulsion; Plasma Physics; Aerospace Engineering; Nuclear Engineering and Radiological Sciences; Engineering

…testing performed at the University of Michigan with a 15 cm ion source. The 15 cm source has… 

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APA (6th Edition):

Arthur, N. (2017). Increasing the Extracted Beam Current Density in Ion Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/140908

Chicago Manual of Style (16th Edition):

Arthur, Neil. “Increasing the Extracted Beam Current Density in Ion Thrusters.” 2017. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/140908.

MLA Handbook (7th Edition):

Arthur, Neil. “Increasing the Extracted Beam Current Density in Ion Thrusters.” 2017. Web. 14 Dec 2019.

Vancouver:

Arthur N. Increasing the Extracted Beam Current Density in Ion Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/140908.

Council of Science Editors:

Arthur N. Increasing the Extracted Beam Current Density in Ion Thrusters. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/140908

24. Durot, Christopher J. Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations.

Degree: PhD, Applied Physics, 2016, University of Michigan

 Time-resolved measurements of ion dynamics could be key to understanding the physics of instabilities, electron transport, and erosion in Hall thrusters. Traditional measurements of the… (more)

Subjects/Keywords: Hall thruster; electric propulsion; transfer function; phase-sensitive detection; diagnostics; laser-induced fluorescence; Aerospace Engineering; Engineering (General); Nuclear Engineering and Radiological Sciences; Physics; Science (General); Engineering; Science

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APA (6th Edition):

Durot, C. J. (2016). Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/133454

Chicago Manual of Style (16th Edition):

Durot, Christopher J. “Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations.” 2016. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/133454.

MLA Handbook (7th Edition):

Durot, Christopher J. “Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations.” 2016. Web. 14 Dec 2019.

Vancouver:

Durot CJ. Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/133454.

Council of Science Editors:

Durot CJ. Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/133454

25. Liang, Raymond. The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Hall-effect thrusters continue to be one of the most efficient technologies for spacecraft maneuvering and stationkeeping. One of the ongoing efforts in the electric propulsion… (more)

Subjects/Keywords: Electric Propulsion; Space Propulsion; Nested Hall Thruster; Aerospace Engineering; Engineering

…TAL Thruster with Anode Layer UM University of Michigan XIPS Xenon Ion Propulsion… …by the University of Michigan and the Air Force Research Laboratory, with later sponsorship… …University of Michigan (UM) and the Air Force Research Laboratory (AFRL)… 

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APA (6th Edition):

Liang, R. (2013). The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/100043

Chicago Manual of Style (16th Edition):

Liang, Raymond. “The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/100043.

MLA Handbook (7th Edition):

Liang, Raymond. “The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster.” 2013. Web. 14 Dec 2019.

Vancouver:

Liang R. The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/100043.

Council of Science Editors:

Liang R. The Combination of Two Concentric Discharge Channels into a Nested Hall-Effect Thruster. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/100043

26. Gamboa, Eliseo J. Spatially-resolved x-ray Scattering Experiments.

Degree: PhD, Applied Physics, 2013, University of Michigan

 In many laboratory astrophysics experiments, intense laser irradiation creates novel material conditions with large, one-dimensional gradients in the temperature, density, and ionization state. X-ray Thomson… (more)

Subjects/Keywords: High-energy Density Physics; Physics; Science

…possible without the contributions of many individuals at the University of Michigan, Los Alamos… …fabricated at the University of Michigan by Sallee Klein, Robb Gillespie, and the author. On the… 

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APA (6th Edition):

Gamboa, E. J. (2013). Spatially-resolved x-ray Scattering Experiments. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/102287

Chicago Manual of Style (16th Edition):

Gamboa, Eliseo J. “Spatially-resolved x-ray Scattering Experiments.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/102287.

MLA Handbook (7th Edition):

Gamboa, Eliseo J. “Spatially-resolved x-ray Scattering Experiments.” 2013. Web. 14 Dec 2019.

Vancouver:

Gamboa EJ. Spatially-resolved x-ray Scattering Experiments. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/102287.

Council of Science Editors:

Gamboa EJ. Spatially-resolved x-ray Scattering Experiments. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/102287

27. Orians, Matt L. Low Power Thermal Reactor for Deep Space Probes.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2013, University of Michigan

 Deep space probes travel too far from the sun to use solar power and thus are dependent on Nuclear Power. Currently this is in the… (more)

Subjects/Keywords: Low Power Thermal Reactor for Deep Space Probes; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Orians, M. L. (2013). Low Power Thermal Reactor for Deep Space Probes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/99964

Chicago Manual of Style (16th Edition):

Orians, Matt L. “Low Power Thermal Reactor for Deep Space Probes.” 2013. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/99964.

MLA Handbook (7th Edition):

Orians, Matt L. “Low Power Thermal Reactor for Deep Space Probes.” 2013. Web. 14 Dec 2019.

Vancouver:

Orians ML. Low Power Thermal Reactor for Deep Space Probes. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/99964.

Council of Science Editors:

Orians ML. Low Power Thermal Reactor for Deep Space Probes. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/99964

28. Choi, Maria. Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects.

Degree: PhD, Aerospace Engineering, 2016, University of Michigan

 Hall-effect thrusters (HETs) are affordable and efficient electric propulsion devices for space exploration, with higher specific impulse than conventional chemical propulsion and higher thrust at… (more)

Subjects/Keywords: Hybrid particle-fluid simulation of a Hall thruster plume; Electron mobility modeling in a Hall thruster plume; Development of a 2-D axisymmetric electron model using the continuous Galerkin finite element method; Effect of a magnetic field in a Hall thruster plume; A sputter model of LaB6 cathode keeper; Aerospace Engineering; Engineering

…and the University of Michigan [8]. The H6 Hall thruster has a nominal operating… …the University of Michigan, and has been used by many others [25, 7, 26] to… 

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APA (6th Edition):

Choi, M. (2016). Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/133320

Chicago Manual of Style (16th Edition):

Choi, Maria. “Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects.” 2016. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/133320.

MLA Handbook (7th Edition):

Choi, Maria. “Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects.” 2016. Web. 14 Dec 2019.

Vancouver:

Choi M. Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/133320.

Council of Science Editors:

Choi M. Improved Hall Thruster Plume Simulation by Including Magnetic Field Effects. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/133320

29. Florenz, Roland Edward. The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance.

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

 There is a demonstrated need within the aerospace community for propulsion units that can accomplish an ever increasing broad range of missions. One such mission,… (more)

Subjects/Keywords: Electric Propulsion; Aerospace Engineering; Engineering

…incorrectness, has been priceless. The staff of the University of Michigan Aerospace Engineering… 

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APA (6th Edition):

Florenz, R. E. (2014). The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/107090

Chicago Manual of Style (16th Edition):

Florenz, Roland Edward. “The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance.” 2014. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/107090.

MLA Handbook (7th Edition):

Florenz, Roland Edward. “The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance.” 2014. Web. 14 Dec 2019.

Vancouver:

Florenz RE. The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/107090.

Council of Science Editors:

Florenz RE. The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/107090

30. Sawlani, Kapil Umesh. Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters.

Degree: PhD, Nuclear Engineering and Radiological Sciences, 2015, University of Michigan

 The nature of plasma transport across the magnetic field in crossed-field (CF) devices such as Hall effect thrusters (HETs) remains largely an unsolved problem. This… (more)

Subjects/Keywords: Electron gun; plasma; secondary electron emission; SEE; Aerospace Engineering; Engineering (General); Materials Science and Engineering; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Sawlani, K. U. (2015). Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/111614

Chicago Manual of Style (16th Edition):

Sawlani, Kapil Umesh. “Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters.” 2015. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/111614.

MLA Handbook (7th Edition):

Sawlani, Kapil Umesh. “Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters.” 2015. Web. 14 Dec 2019.

Vancouver:

Sawlani KU. Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/111614.

Council of Science Editors:

Sawlani KU. Effects of Secondary Electron Emission on the Plasma Sheath and Local Electron Energy Distribution with Application to Hall Thrusters. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/111614

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