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You searched for subject:(electric propulsion). Showing records 1 – 30 of 202 total matches.

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Luleå University of Technology

1. Huarcaya, Victor. Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System.

Degree: 2012, Luleå University of Technology

Originally developed and used for fusion research purposes, an Inertial Electrostatic Confinement (IEC) device is introduced for space propulsion applications. It is described the… (more)

Subjects/Keywords: Technology; Space Propulsion; Electric Propulsion; Teknik

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APA (6th Edition):

Huarcaya, V. (2012). Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44228

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):

Huarcaya, Victor. “Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System.” 2012. Thesis, Luleå University of Technology. Accessed January 23, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44228.

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

MLA Handbook (7th Edition):

Huarcaya, Victor. “Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System.” 2012. Web. 23 Jan 2020.

Vancouver:

Huarcaya V. Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2020 Jan 23]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44228.

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

Council of Science Editors:

Huarcaya V. Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System. [Thesis]. Luleå University of Technology; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44228

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


University of Illinois – Urbana-Champaign

2. Patterson, Andrew Paul. System identification for development of distributed electric propulsion vertical take-off vehicles.

Degree: MS, Mechanical Engineering, 2017, University of Illinois – Urbana-Champaign

 This thesis presents a complete procedure for estimating the inertia matrix of a multi-rotor vertical take-off and landing vehicle. The procedure starts with an overview… (more)

Subjects/Keywords: System identification; Distributed electric propulsion

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APA (6th Edition):

Patterson, A. P. (2017). System identification for development of distributed electric propulsion vertical take-off vehicles. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/97340

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):

Patterson, Andrew Paul. “System identification for development of distributed electric propulsion vertical take-off vehicles.” 2017. Thesis, University of Illinois – Urbana-Champaign. Accessed January 23, 2020. http://hdl.handle.net/2142/97340.

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

MLA Handbook (7th Edition):

Patterson, Andrew Paul. “System identification for development of distributed electric propulsion vertical take-off vehicles.” 2017. Web. 23 Jan 2020.

Vancouver:

Patterson AP. System identification for development of distributed electric propulsion vertical take-off vehicles. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2142/97340.

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

Council of Science Editors:

Patterson AP. System identification for development of distributed electric propulsion vertical take-off vehicles. [Thesis]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/97340

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


University of Illinois – Urbana-Champaign

3. Ahern, Drew. Investigation of a space propulsion concept using inertial electrostatic confinement.

Degree: PhD, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign

 This thesis discusses the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER), a space propulsion concept consisting of a helicon source for plasma generation and an… (more)

Subjects/Keywords: electric propulsion; inertial electrostatic confinement

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APA (6th Edition):

Ahern, D. (2018). Investigation of a space propulsion concept using inertial electrostatic confinement. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/100997

Chicago Manual of Style (16th Edition):

Ahern, Drew. “Investigation of a space propulsion concept using inertial electrostatic confinement.” 2018. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed January 23, 2020. http://hdl.handle.net/2142/100997.

MLA Handbook (7th Edition):

Ahern, Drew. “Investigation of a space propulsion concept using inertial electrostatic confinement.” 2018. Web. 23 Jan 2020.

Vancouver:

Ahern D. Investigation of a space propulsion concept using inertial electrostatic confinement. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2142/100997.

Council of Science Editors:

Ahern D. Investigation of a space propulsion concept using inertial electrostatic confinement. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/100997


Penn State University

4. Hopkins, Jeffrey Robert. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.

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

 The direct thrust output, efficiency, and specific impulse of an 8-GHz microwave electrothermal thruster (MET) was measured using a vertical thrust stand in an evacuated… (more)

Subjects/Keywords: electrothermal; electric propulsion; thrust measurment

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APA (6th Edition):

Hopkins, J. R. (2011). DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/11880

Chicago Manual of Style (16th Edition):

Hopkins, Jeffrey Robert. “DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.” 2011. Masters Thesis, Penn State University. Accessed January 23, 2020. https://etda.libraries.psu.edu/catalog/11880.

MLA Handbook (7th Edition):

Hopkins, Jeffrey Robert. “DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER.” 2011. Web. 23 Jan 2020.

Vancouver:

Hopkins JR. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2020 Jan 23]. Available from: https://etda.libraries.psu.edu/catalog/11880.

Council of Science Editors:

Hopkins JR. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. [Masters Thesis]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/11880


Arizona State University

5. Brunacini, Lauren. Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation.

Degree: Mechanical Engineering, 2019, Arizona State University

 In recent years, a new type of ionic salt based solid propellant, considered inert until the application of an electric current induces an electro-chemical reaction,… (more)

Subjects/Keywords: Aerospace engineering; Electric Propellant; Propulsion

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APA (6th Edition):

Brunacini, L. (2019). Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/53457

Chicago Manual of Style (16th Edition):

Brunacini, Lauren. “Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation.” 2019. Masters Thesis, Arizona State University. Accessed January 23, 2020. http://repository.asu.edu/items/53457.

MLA Handbook (7th Edition):

Brunacini, Lauren. “Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation.” 2019. Web. 23 Jan 2020.

Vancouver:

Brunacini L. Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation. [Internet] [Masters thesis]. Arizona State University; 2019. [cited 2020 Jan 23]. Available from: http://repository.asu.edu/items/53457.

Council of Science Editors:

Brunacini L. Investigation of the Electrical Resistivity of a Perchlorate Oxidizer Based Electric Propellant Formulation. [Masters Thesis]. Arizona State University; 2019. Available from: http://repository.asu.edu/items/53457


Princeton University

6. Feldman, Matthew Solomon. The Direct Wave-Drive Thruster .

Degree: PhD, 2017, Princeton University

 A propulsion concept relying on the direct, steady-state acceleration of a plasma by an inductive wave-launching antenna is presented. By operating inductively in steady state,… (more)

Subjects/Keywords: Electric Propulsion; Electrodeless; Plasma; Waves

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APA (6th Edition):

Feldman, M. S. (2017). The Direct Wave-Drive Thruster . (Doctoral Dissertation). Princeton University. Retrieved from http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k

Chicago Manual of Style (16th Edition):

Feldman, Matthew Solomon. “The Direct Wave-Drive Thruster .” 2017. Doctoral Dissertation, Princeton University. Accessed January 23, 2020. http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k.

MLA Handbook (7th Edition):

Feldman, Matthew Solomon. “The Direct Wave-Drive Thruster .” 2017. Web. 23 Jan 2020.

Vancouver:

Feldman MS. The Direct Wave-Drive Thruster . [Internet] [Doctoral dissertation]. Princeton University; 2017. [cited 2020 Jan 23]. Available from: http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k.

Council of Science Editors:

Feldman MS. The Direct Wave-Drive Thruster . [Doctoral Dissertation]. Princeton University; 2017. Available from: http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k


Northeastern University

7. Hyde, Alexander. Development And Characterization Of Rf-driven Plasma And Uv Light Sources.

Degree: PhD, Department of Physics, 2019, Northeastern University

 The research work contained in this thesis is focused on the experimental and numerical study of radio frequency (RF) gas discharges, as well as the… (more)

Subjects/Keywords: Electric Propulsion; Minihelicon; Plasma; Physics

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APA (6th Edition):

Hyde, A. (2019). Development And Characterization Of Rf-driven Plasma And Uv Light Sources. (Doctoral Dissertation). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20324054

Chicago Manual of Style (16th Edition):

Hyde, Alexander. “Development And Characterization Of Rf-driven Plasma And Uv Light Sources.” 2019. Doctoral Dissertation, Northeastern University. Accessed January 23, 2020. http://hdl.handle.net/2047/D20324054.

MLA Handbook (7th Edition):

Hyde, Alexander. “Development And Characterization Of Rf-driven Plasma And Uv Light Sources.” 2019. Web. 23 Jan 2020.

Vancouver:

Hyde A. Development And Characterization Of Rf-driven Plasma And Uv Light Sources. [Internet] [Doctoral dissertation]. Northeastern University; 2019. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2047/D20324054.

Council of Science Editors:

Hyde A. Development And Characterization Of Rf-driven Plasma And Uv Light Sources. [Doctoral Dissertation]. Northeastern University; 2019. Available from: http://hdl.handle.net/2047/D20324054


Cal Poly

8. McGehee, Will Alan. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  The need for micropropulsion solutions for spacecraft has been steadily increasing as scientific payloads require higher accuracy maneuvers and as the use of small… (more)

Subjects/Keywords: Electrospray; Colloid; Thruster; Propulsion; Micropropulsion; Electric Propulsion; Propulsion and Power

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APA (6th Edition):

McGehee, W. A. (2019). Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93

Chicago Manual of Style (16th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Masters Thesis, Cal Poly. Accessed January 23, 2020. https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93.

MLA Handbook (7th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Web. 23 Jan 2020.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93.

Council of Science Editors:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93


Penn State University

9. Asif, Mohammed. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.

Degree: 2018, Penn State University

 This thesis presents progress on the development of the Miniature Microwave-Frequency Ion Thruster (MMIT), currently being developed at Penn State as a microthruster with high… (more)

Subjects/Keywords: space propulsion; plasma propulsion; propulsion; electric propulsion; rocket propulsion; ion engines; microwave thruster; ion thruster; experimental research on electric propulsion; computational research on electric propulsion; miniaturization of electric propulsion; ion thrusters for CubeSats; electric propulsion for CubeSats

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APA (6th Edition):

Asif, M. (2018). PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/15219mxa310

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):

Asif, Mohammed. “PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Thesis, Penn State University. Accessed January 23, 2020. https://etda.libraries.psu.edu/catalog/15219mxa310.

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

MLA Handbook (7th Edition):

Asif, Mohammed. “PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Web. 23 Jan 2020.

Vancouver:

Asif M. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2020 Jan 23]. Available from: https://etda.libraries.psu.edu/catalog/15219mxa310.

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

Council of Science Editors:

Asif M. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Thesis]. Penn State University; 2018. Available from: https://etda.libraries.psu.edu/catalog/15219mxa310

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


University of Illinois – Urbana-Champaign

10. Thomas, Robert E., II. Development and Testing of a Gallium Electromagnetic (GEM) Thruster.

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

 An ablative, quasi-steady electromagnetic plasma accelerator is tested to quantify various characteristics of its operation. An array of diagnostics are used to characterize a gallium… (more)

Subjects/Keywords: Electric Propulsion: Plasma Diagnostics: Space Propulsion: Pulsed Power

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APA (6th Edition):

Thomas, Robert E., I. (2011). Development and Testing of a Gallium Electromagnetic (GEM) Thruster. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/18547

Chicago Manual of Style (16th Edition):

Thomas, Robert E., II. “Development and Testing of a Gallium Electromagnetic (GEM) Thruster.” 2011. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed January 23, 2020. http://hdl.handle.net/2142/18547.

MLA Handbook (7th Edition):

Thomas, Robert E., II. “Development and Testing of a Gallium Electromagnetic (GEM) Thruster.” 2011. Web. 23 Jan 2020.

Vancouver:

Thomas, Robert E. I. Development and Testing of a Gallium Electromagnetic (GEM) Thruster. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2011. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2142/18547.

Council of Science Editors:

Thomas, Robert E. I. Development and Testing of a Gallium Electromagnetic (GEM) Thruster. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/18547


Virginia Tech

11. Mittal, Shawn. Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 Electrothermal (ET) Plasma Technology has been used for many decades in a wide variety of scientific and industrial applications. Due to its numerous applications and… (more)

Subjects/Keywords: electrothermal plasma; space propulsion; electric weaponry; electrothermal chemical guns; electrothermal propulsion

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APA (6th Edition):

Mittal, S. (2015). Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/52705

Chicago Manual of Style (16th Edition):

Mittal, Shawn. “Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept.” 2015. Masters Thesis, Virginia Tech. Accessed January 23, 2020. http://hdl.handle.net/10919/52705.

MLA Handbook (7th Edition):

Mittal, Shawn. “Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept.” 2015. Web. 23 Jan 2020.

Vancouver:

Mittal S. Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/10919/52705.

Council of Science Editors:

Mittal S. Computational Analysis and Design of the Electrothermal Energetic Plasma Source Concept. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/52705


Univerzitet u Beogradu

12. Иванов, Тони, 1987- 32733287. Оптимизација и интеграција електровентиланторског система пропулзора.

Degree: Mašinski fakultet, 2019, Univerzitet u Beogradu

Машинство - Ваздухопловство / Mechanical engineering - Aerospace Engineering

Растући тренд у погледу истраживања везана за електрични погон није заоби- шао ваздухопловну грану индустрије. Последњих… (more)

Subjects/Keywords: Aircraft propulsion; shape parameterization; metaheuristic methods; electric drive; fan propulsion

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APA (6th Edition):

Иванов, Тони, 1. 3. (2019). Оптимизација и интеграција електровентиланторског система пропулзора. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:20685/bdef:Content/get

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):

Иванов, Тони, 1987- 32733287. “Оптимизација и интеграција електровентиланторског система пропулзора.” 2019. Thesis, Univerzitet u Beogradu. Accessed January 23, 2020. https://fedorabg.bg.ac.rs/fedora/get/o:20685/bdef:Content/get.

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

MLA Handbook (7th Edition):

Иванов, Тони, 1987- 32733287. “Оптимизација и интеграција електровентиланторског система пропулзора.” 2019. Web. 23 Jan 2020.

Vancouver:

Иванов, Тони 13. Оптимизација и интеграција електровентиланторског система пропулзора. [Internet] [Thesis]. Univerzitet u Beogradu; 2019. [cited 2020 Jan 23]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:20685/bdef:Content/get.

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

Council of Science Editors:

Иванов, Тони 13. Оптимизација и интеграција електровентиланторског система пропулзора. [Thesis]. Univerzitet u Beogradu; 2019. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:20685/bdef:Content/get

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


Mississippi State University

13. 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 January 23, 2020. 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. 23 Jan 2020.

Vancouver:

Reneau J. INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE PLASMA ACCELERATION MODEL. [Internet] [Masters thesis]. Mississippi State University; 2011. [cited 2020 Jan 23]. 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/ ;


University of Tennessee – Knoxville

14. Broadbent, Andrew Joseph. Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster.

Degree: MS, Aerospace Engineering, 2018, University of Tennessee – Knoxville

 Capable of carrying small-scale instruments, micro-satellites, often called CubeSats for their shape, provide an excellent platform for a variety of educational and research missions. However,… (more)

Subjects/Keywords: electrospray; electric propulsion; micro propulsion; finite element simulation

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APA (6th Edition):

Broadbent, A. J. (2018). Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/5153

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):

Broadbent, Andrew Joseph. “Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster.” 2018. Thesis, University of Tennessee – Knoxville. Accessed January 23, 2020. https://trace.tennessee.edu/utk_gradthes/5153.

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

MLA Handbook (7th Edition):

Broadbent, Andrew Joseph. “Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster.” 2018. Web. 23 Jan 2020.

Vancouver:

Broadbent AJ. Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster. [Internet] [Thesis]. University of Tennessee – Knoxville; 2018. [cited 2020 Jan 23]. Available from: https://trace.tennessee.edu/utk_gradthes/5153.

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

Council of Science Editors:

Broadbent AJ. Feasibility Study of Laser-Fabricated Micro-Needles as an Electrospray Thruster. [Thesis]. University of Tennessee – Knoxville; 2018. Available from: https://trace.tennessee.edu/utk_gradthes/5153

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

15. 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 January 23, 2020. 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. 23 Jan 2020.

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 2020 Jan 23]. 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


Cal Poly

16. Powaser, Alexander M. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  Colloid thrusters, and electrospray thrusters as a whole, have been around since the 1960s. When they were first developed, the high efficiency and fine… (more)

Subjects/Keywords: electric propulsion; electrospray thruster; colloid thruster; electrostatic thruster; Propulsion and Power

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APA (6th Edition):

Powaser, A. M. (2019). Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39

Chicago Manual of Style (16th Edition):

Powaser, Alexander M. “Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.” 2019. Masters Thesis, Cal Poly. Accessed January 23, 2020. https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39.

MLA Handbook (7th Edition):

Powaser, Alexander M. “Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.” 2019. Web. 23 Jan 2020.

Vancouver:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39.

Council of Science Editors:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39


Cal Poly

17. Danis, Reed. Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Investigation of complex multirotor aerodynamic phenomena via wind tunnel experimentation is becoming extremely important with the rapid progress in advanced distributed propulsion VTOL concepts.… (more)

Subjects/Keywords: Electric Propulsion; Distributed Propulsion; Multirotor; Quadcopter; Wind Tunnel Testing; Aeronautical Vehicles

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APA (6th Edition):

Danis, R. (2018). Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1909 ; 10.15368/theses.2018.63

Chicago Manual of Style (16th Edition):

Danis, Reed. “Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel.” 2018. Masters Thesis, Cal Poly. Accessed January 23, 2020. https://digitalcommons.calpoly.edu/theses/1909 ; 10.15368/theses.2018.63.

MLA Handbook (7th Edition):

Danis, Reed. “Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel.” 2018. Web. 23 Jan 2020.

Vancouver:

Danis R. Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2020 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/1909 ; 10.15368/theses.2018.63.

Council of Science Editors:

Danis R. Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1909 ; 10.15368/theses.2018.63


McMaster University

18. Mahvelatishamsabadi, Parisa. Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles.

Degree: MASc, 2019, McMaster University

Over the past few years, electric propulsion systems have been widely used in automotive applications. The next decade is likely to see the electrification of… (more)

Subjects/Keywords: Electric Propulsion System; ESTOL; Electric motors; Electrified air vehicle; Electric Airplane

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APA (6th Edition):

Mahvelatishamsabadi, P. (2019). Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles. (Masters Thesis). McMaster University. Retrieved from http://hdl.handle.net/11375/24925

Chicago Manual of Style (16th Edition):

Mahvelatishamsabadi, Parisa. “Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles.” 2019. Masters Thesis, McMaster University. Accessed January 23, 2020. http://hdl.handle.net/11375/24925.

MLA Handbook (7th Edition):

Mahvelatishamsabadi, Parisa. “Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles.” 2019. Web. 23 Jan 2020.

Vancouver:

Mahvelatishamsabadi P. Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles. [Internet] [Masters thesis]. McMaster University; 2019. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/11375/24925.

Council of Science Editors:

Mahvelatishamsabadi P. Electric Propulsion System for Exceptionally Short Takeoff and Landing Electric Air Vehicles. [Masters Thesis]. McMaster University; 2019. Available from: http://hdl.handle.net/11375/24925


Loughborough University

19. Patel, Samir N. D. H. Modelling of premixed turbulent propagating flames.

Degree: PhD, 2001, Loughborough University

 Combustion has an active role in our modern lives as we continue to exploit its potential for many of our requirements. For example, its use… (more)

Subjects/Keywords: 541; Electric propulsion

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APA (6th Edition):

Patel, S. N. D. H. (2001). Modelling of premixed turbulent propagating flames. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/6810 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250895

Chicago Manual of Style (16th Edition):

Patel, Samir N D H. “Modelling of premixed turbulent propagating flames.” 2001. Doctoral Dissertation, Loughborough University. Accessed January 23, 2020. https://dspace.lboro.ac.uk/2134/6810 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250895.

MLA Handbook (7th Edition):

Patel, Samir N D H. “Modelling of premixed turbulent propagating flames.” 2001. Web. 23 Jan 2020.

Vancouver:

Patel SNDH. Modelling of premixed turbulent propagating flames. [Internet] [Doctoral dissertation]. Loughborough University; 2001. [cited 2020 Jan 23]. Available from: https://dspace.lboro.ac.uk/2134/6810 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250895.

Council of Science Editors:

Patel SNDH. Modelling of premixed turbulent propagating flames. [Doctoral Dissertation]. Loughborough University; 2001. Available from: https://dspace.lboro.ac.uk/2134/6810 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250895


Penn State University

20. 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 January 23, 2020. 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. 23 Jan 2020.

Vancouver:

Capalungan EE. Design And Development of a 30-GHz Microwave Electrothermal Thruster. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2020 Jan 23]. 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


University of Toronto

21. Gogul, Damon Aaron. Design of a Passively Isolated Novel Thrust Stand (PINTS).

Degree: 2018, University of Toronto

This thesis explores the viability of an inverted pendulum-type thrust stand for measuring forces from low thrust micropropulsion systems. The apparatus is designed around testing… (more)

Subjects/Keywords: Electric; Measurement; Noise; Pendulum; Propulsion; Thrust; 0538

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APA (6th Edition):

Gogul, D. A. (2018). Design of a Passively Isolated Novel Thrust Stand (PINTS). (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/91544

Chicago Manual of Style (16th Edition):

Gogul, Damon Aaron. “Design of a Passively Isolated Novel Thrust Stand (PINTS).” 2018. Masters Thesis, University of Toronto. Accessed January 23, 2020. http://hdl.handle.net/1807/91544.

MLA Handbook (7th Edition):

Gogul, Damon Aaron. “Design of a Passively Isolated Novel Thrust Stand (PINTS).” 2018. Web. 23 Jan 2020.

Vancouver:

Gogul DA. Design of a Passively Isolated Novel Thrust Stand (PINTS). [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/1807/91544.

Council of Science Editors:

Gogul DA. Design of a Passively Isolated Novel Thrust Stand (PINTS). [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/91544


University of Toronto

22. 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 January 23, 2020. 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. 23 Jan 2020.

Vancouver:

Pigeon C. Development of a Miniature Low Power Cylindrical Hall Thruster for Microsatellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2020 Jan 23]. 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


Loughborough University

23. Patel, Samir N. D. H. Modelling of premixed turbulent propagating flames.

Degree: PhD, 2001, Loughborough University

 Combustion has an active role in our modern lives as we continue to exploit its potential for many of our requirements. For example, its use… (more)

Subjects/Keywords: 541; Electric propulsion

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

APA (6th Edition):

Patel, S. N. D. H. (2001). Modelling of premixed turbulent propagating flames. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/6810

Chicago Manual of Style (16th Edition):

Patel, Samir N D H. “Modelling of premixed turbulent propagating flames.” 2001. Doctoral Dissertation, Loughborough University. Accessed January 23, 2020. http://hdl.handle.net/2134/6810.

MLA Handbook (7th Edition):

Patel, Samir N D H. “Modelling of premixed turbulent propagating flames.” 2001. Web. 23 Jan 2020.

Vancouver:

Patel SNDH. Modelling of premixed turbulent propagating flames. [Internet] [Doctoral dissertation]. Loughborough University; 2001. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2134/6810.

Council of Science Editors:

Patel SNDH. Modelling of premixed turbulent propagating flames. [Doctoral Dissertation]. Loughborough University; 2001. Available from: http://hdl.handle.net/2134/6810

24. Little, Justin. Performance Scaling of Magnetic Nozzles for Electric Propulsion .

Degree: PhD, 2015, Princeton University

 The use of magnetic nozzles (MNs) in electric propulsion (EP) systems is investigated analytically and experimentally. MNs have the potential to efficiently accelerate propellant without… (more)

Subjects/Keywords: Electric Propulsion; Helicon Plasma; Magnetic Nozzle

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APA (6th Edition):

Little, J. (2015). Performance Scaling of Magnetic Nozzles for Electric Propulsion . (Doctoral Dissertation). Princeton University. Retrieved from http://arks.princeton.edu/ark:/88435/dsp015712m877m

Chicago Manual of Style (16th Edition):

Little, Justin. “Performance Scaling of Magnetic Nozzles for Electric Propulsion .” 2015. Doctoral Dissertation, Princeton University. Accessed January 23, 2020. http://arks.princeton.edu/ark:/88435/dsp015712m877m.

MLA Handbook (7th Edition):

Little, Justin. “Performance Scaling of Magnetic Nozzles for Electric Propulsion .” 2015. Web. 23 Jan 2020.

Vancouver:

Little J. Performance Scaling of Magnetic Nozzles for Electric Propulsion . [Internet] [Doctoral dissertation]. Princeton University; 2015. [cited 2020 Jan 23]. Available from: http://arks.princeton.edu/ark:/88435/dsp015712m877m.

Council of Science Editors:

Little J. Performance Scaling of Magnetic Nozzles for Electric Propulsion . [Doctoral Dissertation]. Princeton University; 2015. Available from: http://arks.princeton.edu/ark:/88435/dsp015712m877m


Rochester Institute of Technology

25. Sheikh, Ahmed Zia. Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains.

Degree: MS, Sustainability (GIS), 2019, Rochester Institute of Technology

  In the United States, more than a quarter of greenhouse gas (GHGs) emissions (27%) are attributed to the transportation sector which comprises mainly of… (more)

Subjects/Keywords: Electric vehicles; Hybrid propulsion systems; Sustainable mobility

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APA (6th Edition):

Sheikh, A. Z. (2019). Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/10190

Chicago Manual of Style (16th Edition):

Sheikh, Ahmed Zia. “Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains.” 2019. Masters Thesis, Rochester Institute of Technology. Accessed January 23, 2020. https://scholarworks.rit.edu/theses/10190.

MLA Handbook (7th Edition):

Sheikh, Ahmed Zia. “Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains.” 2019. Web. 23 Jan 2020.

Vancouver:

Sheikh AZ. Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains. [Internet] [Masters thesis]. Rochester Institute of Technology; 2019. [cited 2020 Jan 23]. Available from: https://scholarworks.rit.edu/theses/10190.

Council of Science Editors:

Sheikh AZ. Comparative Analysis of Parallel vs Series Hybrid Electric Powertrains. [Masters Thesis]. Rochester Institute of Technology; 2019. Available from: https://scholarworks.rit.edu/theses/10190


University of Missouri – Columbia

26. Olson, Karl M. Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system.

Degree: 2013, University of Missouri – Columbia

 The PTPS-MT consists of a RF driven lithium niobate piezoelectric disc operating as a high voltage step-up transformer to ionize and accelerate plasma in a… (more)

Subjects/Keywords: Electric propulsion; Electrostatic accelerators; Piezoelectricity; Plasma rockets

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APA (6th Edition):

Olson, K. M. (2013). Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system. (Thesis). University of Missouri – Columbia. Retrieved from https://doi.org/10.32469/10355/40208

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):

Olson, Karl M. “Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system.” 2013. Thesis, University of Missouri – Columbia. Accessed January 23, 2020. https://doi.org/10.32469/10355/40208.

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

MLA Handbook (7th Edition):

Olson, Karl M. “Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system.” 2013. Web. 23 Jan 2020.

Vancouver:

Olson KM. Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system. [Internet] [Thesis]. University of Missouri – Columbia; 2013. [cited 2020 Jan 23]. Available from: https://doi.org/10.32469/10355/40208.

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

Council of Science Editors:

Olson KM. Parametric investigation on thrust development of a piezoelectric transformer plasma propulsion system. [Thesis]. University of Missouri – Columbia; 2013. Available from: https://doi.org/10.32469/10355/40208

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


Penn State University

27. 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 January 23, 2020. 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. 23 Jan 2020.

Vancouver:

Hsieh S. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2020 Jan 23]. 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


University of Illinois – Urbana-Champaign

28. Renner, Nathaniel J. Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications.

Degree: MS, Electrical & Computer Engr, 2018, University of Illinois – Urbana-Champaign

 In recent years, advances in power electronics and materials have enabled innovative electric machine (EM) designs. At the same time, the environments and applications in… (more)

Subjects/Keywords: Electric Machines; Design; Qualification; Manufacture; Assembly; Stator Windings; Electric Propulsion

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APA (6th Edition):

Renner, N. J. (2018). Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101043

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):

Renner, Nathaniel J. “Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed January 23, 2020. http://hdl.handle.net/2142/101043.

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

MLA Handbook (7th Edition):

Renner, Nathaniel J. “Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications.” 2018. Web. 23 Jan 2020.

Vancouver:

Renner NJ. Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Jan 23]. Available from: http://hdl.handle.net/2142/101043.

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

Council of Science Editors:

Renner NJ. Development, manufacture, and qualification of stator components for a high-speed electric machine intended for aerospace applications. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101043

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


Florida Atlantic University

29. Sinisterra, Armando Jose. Modeling of linear induction machines for analysis and control.

Degree: M.S.C.S., 2011, Florida Atlantic University

Summary: In this thesis, the analysis of the dynamic response of a Linear Induction Motor as an electromechanical system is done, accounting for all the… (more)

Subjects/Keywords: Electric motors, Induction – Mathematical models; Electric propulsion; Control theory

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APA (6th Edition):

Sinisterra, A. J. (2011). Modeling of linear induction machines for analysis and control. (Masters Thesis). Florida Atlantic University. Retrieved from http://purl.flvc.org/FAU/3172944

Chicago Manual of Style (16th Edition):

Sinisterra, Armando Jose. “Modeling of linear induction machines for analysis and control.” 2011. Masters Thesis, Florida Atlantic University. Accessed January 23, 2020. http://purl.flvc.org/FAU/3172944.

MLA Handbook (7th Edition):

Sinisterra, Armando Jose. “Modeling of linear induction machines for analysis and control.” 2011. Web. 23 Jan 2020.

Vancouver:

Sinisterra AJ. Modeling of linear induction machines for analysis and control. [Internet] [Masters thesis]. Florida Atlantic University; 2011. [cited 2020 Jan 23]. Available from: http://purl.flvc.org/FAU/3172944.

Council of Science Editors:

Sinisterra AJ. Modeling of linear induction machines for analysis and control. [Masters Thesis]. Florida Atlantic University; 2011. Available from: http://purl.flvc.org/FAU/3172944


Michigan Technological University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Hopkins, Mark A. “EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT.” 2015. Doctoral Dissertation, Michigan Technological University. Accessed January 23, 2020. http://digitalcommons.mtu.edu/etds/903.

MLA Handbook (7th Edition):

Hopkins, Mark A. “EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT.” 2015. Web. 23 Jan 2020.

Vancouver:

Hopkins MA. EVALUATION OF MAGNESIUM AS A HALL THRUSTER PROPELLANT. [Internet] [Doctoral dissertation]. Michigan Technological University; 2015. [cited 2020 Jan 23]. Available from: http://digitalcommons.mtu.edu/etds/903.

Council of Science Editors:

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

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