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You searched for subject:(Propulsion AND Power). Showing records 1 – 30 of 140 total matches.

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Delft University of Technology

1. Haseltalab, A. Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control.

Degree: 2019, Delft University of Technology

 In the last few years, autonomous shipping has been under extensive consideration by academic and industrial communities as well as governmental organizations due to several… (more)

Subjects/Keywords: Autonomous ships; DC all-electric; Power and propulsion systems; Model predictive control; Adaptive control

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APA (6th Edition):

Haseltalab, A. (2019). Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 10.4233/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:isbn:978-94-6384-088-0 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73

Chicago Manual of Style (16th Edition):

Haseltalab, A. “Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed January 18, 2020. http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 10.4233/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:isbn:978-94-6384-088-0 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73.

MLA Handbook (7th Edition):

Haseltalab, A. “Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control.” 2019. Web. 18 Jan 2020.

Vancouver:

Haseltalab A. Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2020 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 10.4233/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:isbn:978-94-6384-088-0 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73.

Council of Science Editors:

Haseltalab A. Control for autonomous all-electric ships: Integrating maneuvering, energy management, and power generation control. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 82e02888-5f8d-4936-a33f-b1dcfad53b73 ; 10.4233/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; urn:isbn:978-94-6384-088-0 ; urn:NBN:nl:ui:24-uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73 ; http://resolver.tudelft.nl/uuid:82e02888-5f8d-4936-a33f-b1dcfad53b73


Cal Poly

2. Bughman, Luke J. Modeling and Testing Powerplant Subsystems of a Solar UAS.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  In order to accurately conduct the preliminary and detailed design of solar powered Unmanned Aerial Systems (UAS), it is necessary to have a thorough… (more)

Subjects/Keywords: Solar; UAS; Powerplant; Modeling; Testing; Aeronautical Vehicles; Propulsion and Power

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APA (6th Edition):

Bughman, L. J. (2019). Modeling and Testing Powerplant Subsystems of a Solar UAS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98

Chicago Manual of Style (16th Edition):

Bughman, Luke J. “Modeling and Testing Powerplant Subsystems of a Solar UAS.” 2019. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98.

MLA Handbook (7th Edition):

Bughman, Luke J. “Modeling and Testing Powerplant Subsystems of a Solar UAS.” 2019. Web. 18 Jan 2020.

Vancouver:

Bughman LJ. Modeling and Testing Powerplant Subsystems of a Solar UAS. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98.

Council of Science Editors:

Bughman LJ. Modeling and Testing Powerplant Subsystems of a Solar UAS. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98


Cal Poly

3. 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 18, 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. 18 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 18]. 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


Cal Poly

4. Lunde, Dominic Charles. A Homegrown DSMC-PIC Model for Electric Propulsion.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  Powering spacecraft with electric propulsion is becoming more common, especially in CubeSat-class satellites. On account of the risk of spacecraft interactions, it is important… (more)

Subjects/Keywords: DSMC; PIC; CFD; Plasma; Space; Propulsion; Aerodynamics and Fluid Mechanics; Propulsion and Power; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Lunde, D. C. (2019). A Homegrown DSMC-PIC Model for Electric Propulsion. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48

Chicago Manual of Style (16th Edition):

Lunde, Dominic Charles. “A Homegrown DSMC-PIC Model for Electric Propulsion.” 2019. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48.

MLA Handbook (7th Edition):

Lunde, Dominic Charles. “A Homegrown DSMC-PIC Model for Electric Propulsion.” 2019. Web. 18 Jan 2020.

Vancouver:

Lunde DC. A Homegrown DSMC-PIC Model for Electric Propulsion. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48.

Council of Science Editors:

Lunde DC. A Homegrown DSMC-PIC Model for Electric Propulsion. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48


Cal Poly

5. 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 18, 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. 18 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 18]. 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


Embry-Riddle Aeronautical University

6. Yeung, Tsz Him. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.

Degree: MSin Aerospace Engineering, Graduate Studies, 2019, Embry-Riddle Aeronautical University

  This thesis focuses on electric propulsion technology associated with serial hybrid power plants most commonly associated with urban air mobility vehicles. While closed form… (more)

Subjects/Keywords: Propulsion and Power

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APA (6th Edition):

Yeung, T. H. (2019). Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/457

Chicago Manual of Style (16th Edition):

Yeung, Tsz Him. “Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.” 2019. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 18, 2020. https://commons.erau.edu/edt/457.

MLA Handbook (7th Edition):

Yeung, Tsz Him. “Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.” 2019. Web. 18 Jan 2020.

Vancouver:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2020 Jan 18]. Available from: https://commons.erau.edu/edt/457.

Council of Science Editors:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Masters Thesis]. Embry-Riddle Aeronautical University; 2019. Available from: https://commons.erau.edu/edt/457


Delft University of Technology

7. Geertsma, R.D. Autonomous control for adaptive ships: with hybrid propulsion and power generation.

Degree: 2019, Delft University of Technology

 Shipping plays a crucial role in modern society, but has to reduce its impact on the environment. The commercial availability of power electronic converters and… (more)

Subjects/Keywords: ship propulsion; Non-linear control systems; marine systems; Modelling and simulation; validation; Power systems

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APA (6th Edition):

Geertsma, R. D. (2019). Autonomous control for adaptive ships: with hybrid propulsion and power generation. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; 10.4233/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:isbn:978-90-829766-0-1 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156

Chicago Manual of Style (16th Edition):

Geertsma, R D. “Autonomous control for adaptive ships: with hybrid propulsion and power generation.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed January 18, 2020. http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; 10.4233/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:isbn:978-90-829766-0-1 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156.

MLA Handbook (7th Edition):

Geertsma, R D. “Autonomous control for adaptive ships: with hybrid propulsion and power generation.” 2019. Web. 18 Jan 2020.

Vancouver:

Geertsma RD. Autonomous control for adaptive ships: with hybrid propulsion and power generation. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2020 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; 10.4233/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:isbn:978-90-829766-0-1 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156.

Council of Science Editors:

Geertsma RD. Autonomous control for adaptive ships: with hybrid propulsion and power generation. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; 10.4233/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; urn:isbn:978-90-829766-0-1 ; urn:NBN:nl:ui:24-uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156 ; http://resolver.tudelft.nl/uuid:ad81b0ee-76be-4054-a7e8-bd2eeecdb156


West Virginia University

8. Billups, David Thomas. Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine.

Degree: MS, Mechanical and Aerospace Engineering, 2019, West Virginia University

  Pressure gain combustion (PGC) technologies, specifically rotating detonation engines (RDEs), are poised to provide the next big leap in gas turbine engine advancement, significantly… (more)

Subjects/Keywords: Dimensional analysis; Detonation; Rotating detonation engine; Pressure gain combustion; Dynamic pressure measurement; Aerodynamics and Fluid Mechanics; Energy Systems; Heat Transfer, Combustion; Propulsion and Power

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APA (6th Edition):

Billups, D. T. (2019). Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine. (Thesis). West Virginia University. Retrieved from https://researchrepository.wvu.edu/etd/3774

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):

Billups, David Thomas. “Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine.” 2019. Thesis, West Virginia University. Accessed January 18, 2020. https://researchrepository.wvu.edu/etd/3774.

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

MLA Handbook (7th Edition):

Billups, David Thomas. “Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine.” 2019. Web. 18 Jan 2020.

Vancouver:

Billups DT. Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine. [Internet] [Thesis]. West Virginia University; 2019. [cited 2020 Jan 18]. Available from: https://researchrepository.wvu.edu/etd/3774.

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

Council of Science Editors:

Billups DT. Scaling Analysis and Experimental Investigation of a Rotating Detonation Engine. [Thesis]. West Virginia University; 2019. Available from: https://researchrepository.wvu.edu/etd/3774

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


Michigan Technological University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Masters Thesis, Michigan Technological University. Accessed January 18, 2020. https://digitalcommons.mtu.edu/etdr/886.

MLA Handbook (7th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Web. 18 Jan 2020.

Vancouver:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2019. [cited 2020 Jan 18]. Available from: https://digitalcommons.mtu.edu/etdr/886.

Council of Science Editors:

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


University of Tasmania

10. Shagar, V. Transient suppression in hybrid electric ship power systems.

Degree: 2019, University of Tasmania

 The requirements for power quality in ship power systems have been increasing over the years. This is an essential consequence of improving the efficiency of… (more)

Subjects/Keywords: Power systems; electrical transients; energy storage; hybrid propulsion

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APA (6th Edition):

Shagar, V. (2019). Transient suppression in hybrid electric ship power systems. (Thesis). University of Tasmania. Retrieved from Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania.

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):

Shagar, V. “Transient suppression in hybrid electric ship power systems.” 2019. Thesis, University of Tasmania. Accessed January 18, 2020. Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania..

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

MLA Handbook (7th Edition):

Shagar, V. “Transient suppression in hybrid electric ship power systems.” 2019. Web. 18 Jan 2020.

Vancouver:

Shagar V. Transient suppression in hybrid electric ship power systems. [Internet] [Thesis]. University of Tasmania; 2019. [cited 2020 Jan 18]. Available from: Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania..

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

Council of Science Editors:

Shagar V. Transient suppression in hybrid electric ship power systems. [Thesis]. University of Tasmania; 2019. Available from: Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania.

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


University of Kentucky

11. Flath, Allen, III. Mathematical Programming Approach for the Design of Satellite Power Systems.

Degree: 2019, University of Kentucky

 Satellite power systems can be understood as islanded dc microgrids supplied by specialized and coordinated solar cell arrays augmented by electrochemical battery systems to handle… (more)

Subjects/Keywords: satellite power systems; mathematical model; distributed power generation; modular architectures; multi-period models; Controls and Control Theory; Electrical and Electronics; Power and Energy; Propulsion and Power

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APA (6th Edition):

Flath, Allen, I. (2019). Mathematical Programming Approach for the Design of Satellite Power Systems. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/ece_etds/136

Chicago Manual of Style (16th Edition):

Flath, Allen, III. “Mathematical Programming Approach for the Design of Satellite Power Systems.” 2019. Masters Thesis, University of Kentucky. Accessed January 18, 2020. https://uknowledge.uky.edu/ece_etds/136.

MLA Handbook (7th Edition):

Flath, Allen, III. “Mathematical Programming Approach for the Design of Satellite Power Systems.” 2019. Web. 18 Jan 2020.

Vancouver:

Flath, Allen I. Mathematical Programming Approach for the Design of Satellite Power Systems. [Internet] [Masters thesis]. University of Kentucky; 2019. [cited 2020 Jan 18]. Available from: https://uknowledge.uky.edu/ece_etds/136.

Council of Science Editors:

Flath, Allen I. Mathematical Programming Approach for the Design of Satellite Power Systems. [Masters Thesis]. University of Kentucky; 2019. Available from: https://uknowledge.uky.edu/ece_etds/136


Utah State University

12. Chamberlain, Britany L. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.

Degree: MS, Mechanical and Aerospace Engineering, 2018, Utah State University

  Three-dimensional, additive printing has emerged as an exciting new technology for the design and manufacture of small spacecraft systems. Using 3-D printed thermoplastic materials,… (more)

Subjects/Keywords: hybrid rocket; propulsion; additive manufacturing; CubeSat; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Chamberlain, B. L. (2018). Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7285

Chicago Manual of Style (16th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Masters Thesis, Utah State University. Accessed January 18, 2020. https://digitalcommons.usu.edu/etd/7285.

MLA Handbook (7th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Web. 18 Jan 2020.

Vancouver:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2020 Jan 18]. Available from: https://digitalcommons.usu.edu/etd/7285.

Council of Science Editors:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Masters Thesis]. Utah State University; 2018. Available from: https://digitalcommons.usu.edu/etd/7285

13. Croteau, Tyler J. Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  With an increased demand in Cube Satellite (CubeSat) development for low cost science and exploration missions, a push for the development of micro-propulsion technology… (more)

Subjects/Keywords: Propulsion; Electric Propulsion; Plasma; CubeSat; CFD; Nozzle; Propulsion and Power

…for micro-propulsion options with thrust F , specific impulse Isp , and required power P… …differentiates a propulsion system is its use of electrical power [1, 8]. Split into two… …supply of power for operation, while non-electric, or chemical propulsion systems, may require… …propulsion systems, which may only have < 20 W of total spacecraft power available [5]… …the Pocket Rocket thruster began in the Space Plasma, Power, and Propulsion laboratory at… 

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APA (6th Edition):

Croteau, T. J. (2018). Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143

Chicago Manual of Style (16th Edition):

Croteau, Tyler J. “Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster.” 2018. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143.

MLA Handbook (7th Edition):

Croteau, Tyler J. “Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster.” 2018. Web. 18 Jan 2020.

Vancouver:

Croteau TJ. Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143.

Council of Science Editors:

Croteau TJ. Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143

14. Cinar, Gokcin. A methodology for dynamic sizing of electric power generation and distribution architectures.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Electric and hybrid electric aircraft pose a significant architecture challenge, as these concepts not only deal with considerably high electrical loads, but also are extremely… (more)

Subjects/Keywords: Aircraft design; Electric propulsion; Hybrid propulsion; Electric aircraft; Hybrid aircraft; Subsystem design; Subsystem architecture; Transient analysis; Sizing and synthesis; Power management optimization

power-train for fully electric propulsion 20 2.7 Notional subsystem components and… …Distributed Electric Propulsion . . . . . . . . . 11 viii 2.4 2.5 2.6 2.3.2 Bauhaus Luftfahrt… …Ce-Liner - Electric Propulsion . . . . . . . . . . 13 2.3.3 Boeing SUGAR Volt - Hybrid… …Electric Propulsion . . . . . . . . . . 17 2.3.4 NASA N3X - Turboelectric Propulsion… …71 4.1.5 The Iterative Sizing Process . . . . . . . . . . . . . . . . . . . . . 76 Power… 

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APA (6th Edition):

Cinar, G. (2018). A methodology for dynamic sizing of electric power generation and distribution architectures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60754

Chicago Manual of Style (16th Edition):

Cinar, Gokcin. “A methodology for dynamic sizing of electric power generation and distribution architectures.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2020. http://hdl.handle.net/1853/60754.

MLA Handbook (7th Edition):

Cinar, Gokcin. “A methodology for dynamic sizing of electric power generation and distribution architectures.” 2018. Web. 18 Jan 2020.

Vancouver:

Cinar G. A methodology for dynamic sizing of electric power generation and distribution architectures. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1853/60754.

Council of Science Editors:

Cinar G. A methodology for dynamic sizing of electric power generation and distribution architectures. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60754

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Doctoral Dissertation, Université d'Orléans. Accessed January 18, 2020. http://www.theses.fr/2018ORLE2046.

MLA Handbook (7th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Web. 18 Jan 2020.

Vancouver:

Grimaud L. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. [Internet] [Doctoral dissertation]. Université d'Orléans; 2018. [cited 2020 Jan 18]. Available from: http://www.theses.fr/2018ORLE2046.

Council of Science Editors:

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


Syracuse University

16. Welles, Andrew Voss. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.

Degree: PhD, Mechanical and Aerospace Engineering, 2018, Syracuse University

  This research effort explores the interactions between aerodynamics and hybridelectric power system (HEPS) design and control for vertical takeoff and landing (VTOL) aircraft applications.… (more)

Subjects/Keywords: hybrid power; nonlinear control; power systems; Propulsion; transitional flight; VTOL; Engineering

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APA (6th Edition):

Welles, A. V. (2018). Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/943

Chicago Manual of Style (16th Edition):

Welles, Andrew Voss. “Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.” 2018. Doctoral Dissertation, Syracuse University. Accessed January 18, 2020. https://surface.syr.edu/etd/943.

MLA Handbook (7th Edition):

Welles, Andrew Voss. “Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.” 2018. Web. 18 Jan 2020.

Vancouver:

Welles AV. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. [Internet] [Doctoral dissertation]. Syracuse University; 2018. [cited 2020 Jan 18]. Available from: https://surface.syr.edu/etd/943.

Council of Science Editors:

Welles AV. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. [Doctoral Dissertation]. Syracuse University; 2018. Available from: https://surface.syr.edu/etd/943


Cal Poly

17. King, Harrison Raymond. Electrode Geometry Effects in an Electrothermal Plasma Microthruster.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Nanosatellites, such as Cubesats, are a rapidly growing sector of the space industry. Their popularity stems from their low development cost, short development cycle,… (more)

Subjects/Keywords: Pocket Rocket; capacitive; cubesat; secondary electron; ionization; argon; Propulsion and Power

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APA (6th Edition):

King, H. R. (2018). Electrode Geometry Effects in an Electrothermal Plasma Microthruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73

Chicago Manual of Style (16th Edition):

King, Harrison Raymond. “Electrode Geometry Effects in an Electrothermal Plasma Microthruster.” 2018. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73.

MLA Handbook (7th Edition):

King, Harrison Raymond. “Electrode Geometry Effects in an Electrothermal Plasma Microthruster.” 2018. Web. 18 Jan 2020.

Vancouver:

King HR. Electrode Geometry Effects in an Electrothermal Plasma Microthruster. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73.

Council of Science Editors:

King HR. Electrode Geometry Effects in an Electrothermal Plasma Microthruster. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73


University of Cambridge

18. Alam, Syed Bahauddin. The Design of Reactor Cores for Civil Nuclear Marine Propulsion.

Degree: PhD, 2018, University of Cambridge

 Perhaps surprisingly, the largest experience in operating nuclear power plants has been in nuclear naval propulsion, particularly submarines. This accumulated experience may become the basis… (more)

Subjects/Keywords: Small modular reactor; Soluble-boron-free; neutronics; reactor core design; coupled neutronics/thermal-hydraulics; nuclear marine propulsion; high power density marine core; burnable poison; control rods; Neutron spectrum optimization; Whole-core analysis; Deterministic code; Monte Carlo code; Nodal diffusion method; WIMS; MONK; PANTHER; SERPENT; COBRA-EN

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APA (6th Edition):

Alam, S. B. (2018). The Design of Reactor Cores for Civil Nuclear Marine Propulsion. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/275650

Chicago Manual of Style (16th Edition):

Alam, Syed Bahauddin. “The Design of Reactor Cores for Civil Nuclear Marine Propulsion.” 2018. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2020. https://www.repository.cam.ac.uk/handle/1810/275650.

MLA Handbook (7th Edition):

Alam, Syed Bahauddin. “The Design of Reactor Cores for Civil Nuclear Marine Propulsion.” 2018. Web. 18 Jan 2020.

Vancouver:

Alam SB. The Design of Reactor Cores for Civil Nuclear Marine Propulsion. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2020 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/275650.

Council of Science Editors:

Alam SB. The Design of Reactor Cores for Civil Nuclear Marine Propulsion. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://www.repository.cam.ac.uk/handle/1810/275650


University of Illinois – Urbana-Champaign

19. Pallo, Nathan Andrew. Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft.

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

 The National Aeronautics and Space Administration (NASA), in addition to an increasing number of privately funded ventures, has demonstrated growing interest in more electric aircraft… (more)

Subjects/Keywords: more electric aircraft; flying capacitor; thermal; co-design electrically thin; multilevel; propulsion; hardware-in-the-loop; fault detection; observer; real-time; thermal management; additive manufacturing; heat sink; inverter; high specific power; power density; extreme performance; gallium nitride; wide-bandgap; high efficiency; power converter; dc-dc; dc-ac; electro-thermal

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APA (6th Edition):

Pallo, N. A. (2018). Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101087

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):

Pallo, Nathan Andrew. “Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2020. http://hdl.handle.net/2142/101087.

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

MLA Handbook (7th Edition):

Pallo, Nathan Andrew. “Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft.” 2018. Web. 18 Jan 2020.

Vancouver:

Pallo NA. Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/2142/101087.

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

Council of Science Editors:

Pallo NA. Overcoming electro-thermal barriers to achieve extreme performance power conversion for more electric aircraft. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101087

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


Michigan Technological University

20. Jackson, Brandon. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.

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

  This dissertation presents three studies on the electrospray of ionic liquid ferrofluid. Ionic liquid ferrofluids are electrically conductive super-paramagnetic fluids which respond strongly in… (more)

Subjects/Keywords: ferrofluid; electrospray; ionic liquid; electric satellite propulsion; ferromagnetisim; Other Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Jackson, B. (2018). Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. (Doctoral Dissertation). Michigan Technological University. Retrieved from http://digitalcommons.mtu.edu/etdr/587

Chicago Manual of Style (16th Edition):

Jackson, Brandon. “Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.” 2018. Doctoral Dissertation, Michigan Technological University. Accessed January 18, 2020. http://digitalcommons.mtu.edu/etdr/587.

MLA Handbook (7th Edition):

Jackson, Brandon. “Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.” 2018. Web. 18 Jan 2020.

Vancouver:

Jackson B. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. [Internet] [Doctoral dissertation]. Michigan Technological University; 2018. [cited 2020 Jan 18]. Available from: http://digitalcommons.mtu.edu/etdr/587.

Council of Science Editors:

Jackson B. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. [Doctoral Dissertation]. Michigan Technological University; 2018. Available from: http://digitalcommons.mtu.edu/etdr/587

21. Chikelu, Jennifer Onyinye. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.

Degree: MS, Mechanical Engineering, 2018, South Dakota State University

  Computational fluid dynamics tool has been employed in the past to determine and analyze efficiency or performance in combustion engines and for combustion analysis.… (more)

Subjects/Keywords: Energy Systems; Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Chikelu, J. O. (2018). Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. (Masters Thesis). South Dakota State University. Retrieved from https://openprairie.sdstate.edu/etd/2953

Chicago Manual of Style (16th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Masters Thesis, South Dakota State University. Accessed January 18, 2020. https://openprairie.sdstate.edu/etd/2953.

MLA Handbook (7th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Web. 18 Jan 2020.

Vancouver:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Internet] [Masters thesis]. South Dakota State University; 2018. [cited 2020 Jan 18]. Available from: https://openprairie.sdstate.edu/etd/2953.

Council of Science Editors:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Masters Thesis]. South Dakota State University; 2018. Available from: https://openprairie.sdstate.edu/etd/2953


University of Kentucky

22. Grib, Stephen William. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.

Degree: 2018, University of Kentucky

 Practical gas turbine engine combustors create extremely non-uniform flowfields, which are highly stratified making it imperative that similar environments are well understood. Laser diagnostics were… (more)

Subjects/Keywords: Laser Diagnostics; Edge Flames; Autoignition; Flame Stabilization; Extinction; Heat Transfer, Combustion; Propulsion and Power

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APA (6th Edition):

Grib, S. W. (2018). LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. (Doctoral Dissertation). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/117

Chicago Manual of Style (16th Edition):

Grib, Stephen William. “LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.” 2018. Doctoral Dissertation, University of Kentucky. Accessed January 18, 2020. https://uknowledge.uky.edu/me_etds/117.

MLA Handbook (7th Edition):

Grib, Stephen William. “LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.” 2018. Web. 18 Jan 2020.

Vancouver:

Grib SW. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. [Internet] [Doctoral dissertation]. University of Kentucky; 2018. [cited 2020 Jan 18]. Available from: https://uknowledge.uky.edu/me_etds/117.

Council of Science Editors:

Grib SW. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. [Doctoral Dissertation]. University of Kentucky; 2018. Available from: https://uknowledge.uky.edu/me_etds/117

23. 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

Propulsion . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.1 Province… …of EP Systems in Excess of 300 kW . . . . . . 3.2.1 Progress in On-Board Power… …Electric Propulsion System Mass and 3.4.2 Modifications to Mass Model to Capture NHTs . . 3.4.3… …4.4.3 Power . . . . . . . . . . . . . . . . . . 4.4.4 Telemetry… …88 89 89 91 93 93 97 98 98 98 100 100 101 118 124 124 125 128 137 138 142 5 Low-Power… 

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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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Hall S. Characterization of a 100-kW Class Nested-Channel Hall Thruster. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2020 Jan 18]. 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


University of Michigan

24. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Dragnea H. Development and Application of Multidimensional Computational Models for Hall Thrusters. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2020 Jan 18]. 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 Toronto

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

Degree: 2017, University of Toronto

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Masters Thesis, University of Toronto. Accessed January 18, 2020. http://hdl.handle.net/1807/79053.

MLA Handbook (7th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Web. 18 Jan 2020.

Vancouver:

Svatos AL. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1807/79053.

Council of Science Editors:

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


Cleveland State University

26. Dinca, Dragos. Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications.

Degree: Doctor of Engineering, Washkewicz College of Engineering, 2017, Cleveland State University

 High Intensity Laser Power Beaming is a wireless power transmission technology developed at the Industrial Space Systems Laboratory from 2005 through 2010, in collaboration with… (more)

Subjects/Keywords: Electrical Engineering; Hybrid energy storage; ultracapacitor; battery; power system optimization; laser power beaming; vertical multi-junction solar cells; wireless power transmission; laser; photovoltaic; high intensity lasers; electric propulsion; unmanned air vehicles

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APA (6th Edition):

Dinca, D. (2017). Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications. (Doctoral Dissertation). Cleveland State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=csu1495115874616384

Chicago Manual of Style (16th Edition):

Dinca, Dragos. “Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications.” 2017. Doctoral Dissertation, Cleveland State University. Accessed January 18, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=csu1495115874616384.

MLA Handbook (7th Edition):

Dinca, Dragos. “Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications.” 2017. Web. 18 Jan 2020.

Vancouver:

Dinca D. Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications. [Internet] [Doctoral dissertation]. Cleveland State University; 2017. [cited 2020 Jan 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1495115874616384.

Council of Science Editors:

Dinca D. Development of an Integrated High Energy Density Capture and Storage System for Ultrafast Supply/Extended Energy Consumption Applications. [Doctoral Dissertation]. Cleveland State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1495115874616384


University of Washington

27. Murakami, Nao. High-Power Helicon Double Gun Thruster.

Degree: 2017, University of Washington

 While chemical propulsion is necessary to launch a spacecraft from a planetary surface into space, electric propulsion has the potential to provide significant cost savings… (more)

Subjects/Keywords: Digital Filtering Algorithm; Helicon Thruster; High-Power System; Plasma Physics; Space Propulsion; Aerospace engineering; Plasma physics; Aeronautics and astronautics

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

APA (6th Edition):

Murakami, N. (2017). High-Power Helicon Double Gun Thruster. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/38569

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):

Murakami, Nao. “High-Power Helicon Double Gun Thruster.” 2017. Thesis, University of Washington. Accessed January 18, 2020. http://hdl.handle.net/1773/38569.

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

MLA Handbook (7th Edition):

Murakami, Nao. “High-Power Helicon Double Gun Thruster.” 2017. Web. 18 Jan 2020.

Vancouver:

Murakami N. High-Power Helicon Double Gun Thruster. [Internet] [Thesis]. University of Washington; 2017. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1773/38569.

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

Council of Science Editors:

Murakami N. High-Power Helicon Double Gun Thruster. [Thesis]. University of Washington; 2017. Available from: http://hdl.handle.net/1773/38569

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

28. Oo, Htet Htet Nwe. Actuator Disk Theory for Compressible Flow.

Degree: MS, Mechanical Engineering, 2017, Cal Poly

  Because compressibility effects arise in real applications of propellers and turbines, the Actuator Disk Theory or Froude’s Momentum Theory was established for compressible, subsonic… (more)

Subjects/Keywords: Actuator Disk Theory; Froude's Momentum Theory; compressible flow; turbine; Betz limit; duct; Aerodynamics and Fluid Mechanics; Propulsion and Power

…bare propeller obtained at the maximum power coefficient before the flow is sonic at station… …11 Figure 4. Propulsive efficiency versus the power coefficient between the ducted and bare… …21 Figure 9. Comparison of the power extraction efficiency and the Betz limit between the… …44 Figure 17. The plot gives the maximum power coefficient to drive the propeller before… …65 Figure 32. The plot gives the maximum power coefficient to drive the propeller before… 

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

APA (6th Edition):

Oo, H. H. N. (2017). Actuator Disk Theory for Compressible Flow. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1727 ; 10.15368/theses.2017.28

Chicago Manual of Style (16th Edition):

Oo, Htet Htet Nwe. “Actuator Disk Theory for Compressible Flow.” 2017. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/1727 ; 10.15368/theses.2017.28.

MLA Handbook (7th Edition):

Oo, Htet Htet Nwe. “Actuator Disk Theory for Compressible Flow.” 2017. Web. 18 Jan 2020.

Vancouver:

Oo HHN. Actuator Disk Theory for Compressible Flow. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1727 ; 10.15368/theses.2017.28.

Council of Science Editors:

Oo HHN. Actuator Disk Theory for Compressible Flow. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1727 ; 10.15368/theses.2017.28

29. Baris, Engin. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.

Degree: MS, Mechanical & Aerospace Engineering, 2017, Old Dominion University

  Distributed electric propulsion systems benefit from the inherent scale independence of electric propulsion. This property allows the designer to place multiple small electric motors… (more)

Subjects/Keywords: Design of experiments; Distributed; Electric; Low Reynolds; Propulsion; Small UAV; Aerospace Engineering; Propulsion and Power

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

APA (6th Edition):

Baris, E. (2017). An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. (Thesis). Old Dominion University. Retrieved from 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

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):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Thesis, Old Dominion University. Accessed January 18, 2020. 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

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

MLA Handbook (7th Edition):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Web. 18 Jan 2020.

Vancouver:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Internet] [Thesis]. Old Dominion University; 2017. [cited 2020 Jan 18]. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

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

Council of Science Editors:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Thesis]. Old Dominion University; 2017. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

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


Michigan Technological University

30. Terhune, Kurt Joseph. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.

Degree: PhD, Department of Mechanical Engineering-Engineering Mechanics, 2017, Michigan Technological University

  Two electrospray sources were developed to operate on an ionic liquid ferrofluid; one source was a pressure‑fed capillary electrospray source and the other was… (more)

Subjects/Keywords: Electrospray; ferrofluid; ionic liquid; mass spectrometry; ionic liquid ferrofluid; Analytical Chemistry; Other Engineering; Other Mechanical Engineering; Propulsion and Power

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

APA (6th Edition):

Terhune, K. J. (2017). Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. (Doctoral Dissertation). Michigan Technological University. Retrieved from http://digitalcommons.mtu.edu/etdr/547

Chicago Manual of Style (16th Edition):

Terhune, Kurt Joseph. “Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.” 2017. Doctoral Dissertation, Michigan Technological University. Accessed January 18, 2020. http://digitalcommons.mtu.edu/etdr/547.

MLA Handbook (7th Edition):

Terhune, Kurt Joseph. “Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.” 2017. Web. 18 Jan 2020.

Vancouver:

Terhune KJ. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. [Internet] [Doctoral dissertation]. Michigan Technological University; 2017. [cited 2020 Jan 18]. Available from: http://digitalcommons.mtu.edu/etdr/547.

Council of Science Editors:

Terhune KJ. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. [Doctoral Dissertation]. Michigan Technological University; 2017. Available from: http://digitalcommons.mtu.edu/etdr/547

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