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You searched for subject:(Propulsion). Showing records 1 – 30 of 833 total matches.

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Rutgers University

1. Maia, Marco M., 1990-. Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion.

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

Multi-medium vehicles, which are capable of operating in multiple fluid mediums such as air and water, are a new paradigm in unmanned systems and the… (more)

Subjects/Keywords: Propulsion systems

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APA (6th Edition):

Maia, Marco M., 1. (2018). Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion. (Doctoral Dissertation). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/56054/

Chicago Manual of Style (16th Edition):

Maia, Marco M., 1990-. “Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion.” 2018. Doctoral Dissertation, Rutgers University. Accessed October 15, 2019. https://rucore.libraries.rutgers.edu/rutgers-lib/56054/.

MLA Handbook (7th Edition):

Maia, Marco M., 1990-. “Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion.” 2018. Web. 15 Oct 2019.

Vancouver:

Maia, Marco M. 1. Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion. [Internet] [Doctoral dissertation]. Rutgers University; 2018. [cited 2019 Oct 15]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/56054/.

Council of Science Editors:

Maia, Marco M. 1. Control of a highly maneuverable multi-medium vehicle employing multi-plane propulsion. [Doctoral Dissertation]. Rutgers University; 2018. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/56054/

2. Tran, Phu Ho. Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms.

Degree: Docteur es, Energétique, thermique, combustion, 2013, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique

La caractérisation et la simulation des écoulements internes au sein des moteurs àpropergol solide, en considérant des mécanismes physiques fortement couplés, constituentl’objectif principal de ce… (more)

Subjects/Keywords: Propulsion; Frontières mobiles; Propulsion; Moving boundary

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APA (6th Edition):

Tran, P. H. (2013). Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms. (Doctoral Dissertation). Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Retrieved from http://www.theses.fr/2013ESMA0030

Chicago Manual of Style (16th Edition):

Tran, Phu Ho. “Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms.” 2013. Doctoral Dissertation, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Accessed October 15, 2019. http://www.theses.fr/2013ESMA0030.

MLA Handbook (7th Edition):

Tran, Phu Ho. “Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms.” 2013. Web. 15 Oct 2019.

Vancouver:

Tran PH. Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms. [Internet] [Doctoral dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. [cited 2019 Oct 15]. Available from: http://www.theses.fr/2013ESMA0030.

Council of Science Editors:

Tran PH. Analyse numérique des écoulements internes au sein des moteurs à propergol solide. Vers une prise en compte des mécanismes instationnaires couplés : Numerical analysis of internal flow within the solid rocket motors. To a consideration of coupling unsteady mechanisms. [Doctoral Dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. Available from: http://www.theses.fr/2013ESMA0030


Luleå University of Technology

3. 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 October 15, 2019. 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. 15 Oct 2019.

Vancouver:

Huarcaya V. Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2019 Oct 15]. 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 Tennessee – Knoxville

4. Sung, Rayne. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.

Degree: MS, Aerospace Engineering, 2013, University of Tennessee – Knoxville

  GasTurb 11 and the Gas Turbine Simulation Program (GSP) 11 are two commercially available gas turbine simulation programs used by industrial professionals and academic… (more)

Subjects/Keywords: Propulsion; Turbojet Engine; Thermodynamics; Propulsion and Power

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APA (6th Edition):

Sung, R. (2013). A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2466

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):

Sung, Rayne. “A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.” 2013. Thesis, University of Tennessee – Knoxville. Accessed October 15, 2019. https://trace.tennessee.edu/utk_gradthes/2466.

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

MLA Handbook (7th Edition):

Sung, Rayne. “A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.” 2013. Web. 15 Oct 2019.

Vancouver:

Sung R. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. [Internet] [Thesis]. University of Tennessee – Knoxville; 2013. [cited 2019 Oct 15]. Available from: https://trace.tennessee.edu/utk_gradthes/2466.

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

Council of Science Editors:

Sung R. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. [Thesis]. University of Tennessee – Knoxville; 2013. Available from: https://trace.tennessee.edu/utk_gradthes/2466

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

5. Du Pontavice, Emmanuel. Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander.

Degree: Docteur es, Mécanique des fluides, 2016, Paris Saclay

Les cerf-volants existent depuis l'Antiquité, mais leur utilisation comme moyen de récupération de l'énergie éolienne est relativement récente. Pourtant, leur légèreté et leur capacité à… (more)

Subjects/Keywords: Cerf-Volant; Propulsion; Stabilité; Kite; Propulsion; Stability

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APA (6th Edition):

Du Pontavice, E. (2016). Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2016SACLX015

Chicago Manual of Style (16th Edition):

Du Pontavice, Emmanuel. “Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander.” 2016. Doctoral Dissertation, Paris Saclay. Accessed October 15, 2019. http://www.theses.fr/2016SACLX015.

MLA Handbook (7th Edition):

Du Pontavice, Emmanuel. “Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander.” 2016. Web. 15 Oct 2019.

Vancouver:

Du Pontavice E. Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander. [Internet] [Doctoral dissertation]. Paris Saclay; 2016. [cited 2019 Oct 15]. Available from: http://www.theses.fr/2016SACLX015.

Council of Science Editors:

Du Pontavice E. Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander. [Doctoral Dissertation]. Paris Saclay; 2016. Available from: http://www.theses.fr/2016SACLX015


Delft University of Technology

6. Wijnans, A.S. Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:.

Degree: 2012, Delft University of Technology

 Space debris is becoming an increasing problem requiring a low cost propulsion system capable of disposing non operable satellites and spent rocket stages. To this… (more)

Subjects/Keywords: electrodynamic; tether; propulsion

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APA (6th Edition):

Wijnans, A. S. (2012). Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:437869ae-2a7d-40aa-b809-67b314dc91a7

Chicago Manual of Style (16th Edition):

Wijnans, A S. “Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:.” 2012. Masters Thesis, Delft University of Technology. Accessed October 15, 2019. http://resolver.tudelft.nl/uuid:437869ae-2a7d-40aa-b809-67b314dc91a7.

MLA Handbook (7th Edition):

Wijnans, A S. “Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:.” 2012. Web. 15 Oct 2019.

Vancouver:

Wijnans AS. Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2019 Oct 15]. Available from: http://resolver.tudelft.nl/uuid:437869ae-2a7d-40aa-b809-67b314dc91a7.

Council of Science Editors:

Wijnans AS. Electrodynamic Tether Experiment onboard the Delfi-1 Satellite:. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:437869ae-2a7d-40aa-b809-67b314dc91a7


Embry-Riddle Aeronautical University

7. 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 October 15, 2019. 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. 15 Oct 2019.

Vancouver:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2019 Oct 15]. 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


Cal Poly

8. Green, Michael W. HAPSS, Hybrid Aircraft Propulsion System Synthesis.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Hybrid Aircraft Propulsion System Synthesis (HAPSS) is a computer program that sizes and analyzes pure-series hybrid electric propulsion systems for aircraft. The development of… (more)

Subjects/Keywords: Propulsion and Power

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APA (6th Edition):

Green, M. W. (2012). HAPSS, Hybrid Aircraft Propulsion System Synthesis. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134

Chicago Manual of Style (16th Edition):

Green, Michael W. “HAPSS, Hybrid Aircraft Propulsion System Synthesis.” 2012. Masters Thesis, Cal Poly. Accessed October 15, 2019. https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134.

MLA Handbook (7th Edition):

Green, Michael W. “HAPSS, Hybrid Aircraft Propulsion System Synthesis.” 2012. Web. 15 Oct 2019.

Vancouver:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Oct 15]. Available from: https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134.

Council of Science Editors:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134


San Jose State University

9. Boronowsky, Kenny Michael. Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment.

Degree: MS, Mechanical and Aerospace Engineering, 2011, San Jose State University

  A concept was developed and tested to enhance the performance and regression rate of hydroxyl terminated polybutadiene (HTPB), a commonly used hybrid rocket fuel.… (more)

Subjects/Keywords: Hybrid; Propulsion; Rocketry

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APA (6th Edition):

Boronowsky, K. M. (2011). Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.t2xh-cjwv ; https://scholarworks.sjsu.edu/etd_theses/4039

Chicago Manual of Style (16th Edition):

Boronowsky, Kenny Michael. “Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment.” 2011. Masters Thesis, San Jose State University. Accessed October 15, 2019. https://doi.org/10.31979/etd.t2xh-cjwv ; https://scholarworks.sjsu.edu/etd_theses/4039.

MLA Handbook (7th Edition):

Boronowsky, Kenny Michael. “Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment.” 2011. Web. 15 Oct 2019.

Vancouver:

Boronowsky KM. Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment. [Internet] [Masters thesis]. San Jose State University; 2011. [cited 2019 Oct 15]. Available from: https://doi.org/10.31979/etd.t2xh-cjwv ; https://scholarworks.sjsu.edu/etd_theses/4039.

Council of Science Editors:

Boronowsky KM. Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment. [Masters Thesis]. San Jose State University; 2011. Available from: https://doi.org/10.31979/etd.t2xh-cjwv ; https://scholarworks.sjsu.edu/etd_theses/4039


Cal Poly

10. 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

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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

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 October 15, 2019. https://digitalcommons.calpoly.edu/theses/1961.

MLA Handbook (7th Edition):

Croteau, Tyler J. “MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER.” 2018. Web. 15 Oct 2019.

Vancouver:

Croteau TJ. MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Oct 15]. Available from: https://digitalcommons.calpoly.edu/theses/1961.

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


Cal Poly

11. 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

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 October 15, 2019. https://digitalcommons.calpoly.edu/theses/2064.

MLA Handbook (7th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Web. 15 Oct 2019.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2019 Oct 15]. Available from: https://digitalcommons.calpoly.edu/theses/2064.

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


Embry-Riddle Aeronautical University

12. Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  Pressure gain combustion has been known to be more thermodynamically efficient than its constant pressure counterpart, which employs deflagration. Integration of pressure gain combustors… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Espa˜na-Heredia, L. E. F. (2014). Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from http://commons.erau.edu/edt/158

Chicago Manual of Style (16th Edition):

Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. “Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed October 15, 2019. http://commons.erau.edu/edt/158.

MLA Handbook (7th Edition):

Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. “Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.” 2014. Web. 15 Oct 2019.

Vancouver:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2019 Oct 15]. Available from: http://commons.erau.edu/edt/158.

Council of Science Editors:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: http://commons.erau.edu/edt/158


Texas A&M University

13. Appel, Bradley. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.

Degree: 2012, Texas A&M University

 The goal of this research is to apply modern methods of analysis to the design of a tungsten-cermet Nuclear Thermal Rocket (NTR) core. An NTR… (more)

Subjects/Keywords: nuclear; rocket; CFD; propulsion

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APA (6th Edition):

Appel, B. (2012). Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649

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):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Thesis, Texas A&M University. Accessed October 15, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

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

MLA Handbook (7th Edition):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Web. 15 Oct 2019.

Vancouver:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

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

Council of Science Editors:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649

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


Coventry University

14. Sivapragasam, M. Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns.

Degree: PhD, 2014, Coventry University

 The performance of an aircraft gas turbine engine is adversely affected by the non-uniform or distorted flow in the inlet duct. Inlet flow distortion lowers… (more)

Subjects/Keywords: 629.134; Jet engines; Jet propulsion

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APA (6th Edition):

Sivapragasam, M. (2014). Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns. (Doctoral Dissertation). Coventry University. Retrieved from http://curve.coventry.ac.uk/open/items/0ad1d0c2-6693-4c6e-9224-5a2237862074/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.681405

Chicago Manual of Style (16th Edition):

Sivapragasam, M. “Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns.” 2014. Doctoral Dissertation, Coventry University. Accessed October 15, 2019. http://curve.coventry.ac.uk/open/items/0ad1d0c2-6693-4c6e-9224-5a2237862074/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.681405.

MLA Handbook (7th Edition):

Sivapragasam, M. “Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns.” 2014. Web. 15 Oct 2019.

Vancouver:

Sivapragasam M. Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns. [Internet] [Doctoral dissertation]. Coventry University; 2014. [cited 2019 Oct 15]. Available from: http://curve.coventry.ac.uk/open/items/0ad1d0c2-6693-4c6e-9224-5a2237862074/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.681405.

Council of Science Editors:

Sivapragasam M. Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns. [Doctoral Dissertation]. Coventry University; 2014. Available from: http://curve.coventry.ac.uk/open/items/0ad1d0c2-6693-4c6e-9224-5a2237862074/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.681405


Oregon State University

15. Lockwood, Raymond Marshall. Pulsejet ejectors.

Degree: MS, Mechanical Engineering, 1953, Oregon State University

Subjects/Keywords: Jet propulsion

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APA (6th Edition):

Lockwood, R. M. (1953). Pulsejet ejectors. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/51493

Chicago Manual of Style (16th Edition):

Lockwood, Raymond Marshall. “Pulsejet ejectors.” 1953. Masters Thesis, Oregon State University. Accessed October 15, 2019. http://hdl.handle.net/1957/51493.

MLA Handbook (7th Edition):

Lockwood, Raymond Marshall. “Pulsejet ejectors.” 1953. Web. 15 Oct 2019.

Vancouver:

Lockwood RM. Pulsejet ejectors. [Internet] [Masters thesis]. Oregon State University; 1953. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/1957/51493.

Council of Science Editors:

Lockwood RM. Pulsejet ejectors. [Masters Thesis]. Oregon State University; 1953. Available from: http://hdl.handle.net/1957/51493


Case Western Reserve University

16. Connolly, Joseph W. SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION.

Degree: MSs (Engineering), EECS - System and Control Engineering, 2009, Case Western Reserve University

 Under the NASA Fundamental Aeronautics Program the Supersonics Project aims to overcome the obstacles associated with supersonic commercial flight. The proposed vehicles are long slim… (more)

Subjects/Keywords: Engineering; Supersonics; Propulsion; Aeronautics

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APA (6th Edition):

Connolly, J. W. (2009). SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION. (Masters Thesis). Case Western Reserve University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610

Chicago Manual of Style (16th Edition):

Connolly, Joseph W. “SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION.” 2009. Masters Thesis, Case Western Reserve University. Accessed October 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610.

MLA Handbook (7th Edition):

Connolly, Joseph W. “SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION.” 2009. Web. 15 Oct 2019.

Vancouver:

Connolly JW. SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION. [Internet] [Masters thesis]. Case Western Reserve University; 2009. [cited 2019 Oct 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610.

Council of Science Editors:

Connolly JW. SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION. [Masters Thesis]. Case Western Reserve University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610


Penn State University

17. 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 October 15, 2019. 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. 15 Oct 2019.

Vancouver:

Hopkins JR. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2019 Oct 15]. 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


Penn State University

18. Paunescu, Cristian. Investigation of electromagnetic acceleration of nonionized gases.

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

 Electric propulsion methods have always relied on the interactions between charged particles and electromagnetic fields and, as such, have the shortfall of requiring energy to… (more)

Subjects/Keywords: polar propulsion; Abraham effect

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APA (6th Edition):

Paunescu, C. (2009). Investigation of electromagnetic acceleration of nonionized gases. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9623

Chicago Manual of Style (16th Edition):

Paunescu, Cristian. “Investigation of electromagnetic acceleration of nonionized gases.” 2009. Masters Thesis, Penn State University. Accessed October 15, 2019. https://etda.libraries.psu.edu/catalog/9623.

MLA Handbook (7th Edition):

Paunescu, Cristian. “Investigation of electromagnetic acceleration of nonionized gases.” 2009. Web. 15 Oct 2019.

Vancouver:

Paunescu C. Investigation of electromagnetic acceleration of nonionized gases. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Oct 15]. Available from: https://etda.libraries.psu.edu/catalog/9623.

Council of Science Editors:

Paunescu C. Investigation of electromagnetic acceleration of nonionized gases. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9623


Oregon State University

19. Henry, Calvin Scott. The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream.

Degree: MS, Mechanical Engineering, 1959, Oregon State University

Subjects/Keywords: Jet propulsion

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APA (6th Edition):

Henry, C. S. (1959). The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/50401

Chicago Manual of Style (16th Edition):

Henry, Calvin Scott. “The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream.” 1959. Masters Thesis, Oregon State University. Accessed October 15, 2019. http://hdl.handle.net/1957/50401.

MLA Handbook (7th Edition):

Henry, Calvin Scott. “The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream.” 1959. Web. 15 Oct 2019.

Vancouver:

Henry CS. The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream. [Internet] [Masters thesis]. Oregon State University; 1959. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/1957/50401.

Council of Science Editors:

Henry CS. The development of the characteristic grid for supersonic diverging jets exhausting into a hypersonic parallel flowing stream. [Masters Thesis]. Oregon State University; 1959. Available from: http://hdl.handle.net/1957/50401

20. Shimauchi, Tomoki. Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings.

Degree: PhD, 1980, Imperial College London

Subjects/Keywords: 621.4; Propulsion

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APA (6th Edition):

Shimauchi, T. (1980). Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings. (Doctoral Dissertation). Imperial College London. Retrieved from http://hdl.handle.net/10044/1/35344

Chicago Manual of Style (16th Edition):

Shimauchi, Tomoki. “Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings.” 1980. Doctoral Dissertation, Imperial College London. Accessed October 15, 2019. http://hdl.handle.net/10044/1/35344.

MLA Handbook (7th Edition):

Shimauchi, Tomoki. “Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings.” 1980. Web. 15 Oct 2019.

Vancouver:

Shimauchi T. Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings. [Internet] [Doctoral dissertation]. Imperial College London; 1980. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/10044/1/35344.

Council of Science Editors:

Shimauchi T. Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings. [Doctoral Dissertation]. Imperial College London; 1980. Available from: http://hdl.handle.net/10044/1/35344


Luleå University of Technology

21. Carlsvärd, Fredric. Experimental Test Rig Design and Testing of a Box-Bladed Propeller.

Degree: 2013, Luleå University of Technology

This masters thesis is a dedicated nal work of an aerospace engineering eduction providedby Lule_a University of Technology. The work has been part of… (more)

Subjects/Keywords: Technology; Aerospace; propulsion; testing; Teknik

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APA (6th Edition):

Carlsvärd, F. (2013). Experimental Test Rig Design and Testing of a Box-Bladed Propeller. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57785

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):

Carlsvärd, Fredric. “Experimental Test Rig Design and Testing of a Box-Bladed Propeller.” 2013. Thesis, Luleå University of Technology. Accessed October 15, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57785.

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

MLA Handbook (7th Edition):

Carlsvärd, Fredric. “Experimental Test Rig Design and Testing of a Box-Bladed Propeller.” 2013. Web. 15 Oct 2019.

Vancouver:

Carlsvärd F. Experimental Test Rig Design and Testing of a Box-Bladed Propeller. [Internet] [Thesis]. Luleå University of Technology; 2013. [cited 2019 Oct 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57785.

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

Council of Science Editors:

Carlsvärd F. Experimental Test Rig Design and Testing of a Box-Bladed Propeller. [Thesis]. Luleå University of Technology; 2013. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-57785

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


Delft University of Technology

22. Van der Ham, B. Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :.

Degree: 2015, Delft University of Technology

 Trough developments the wheelchair has become lighter and has less rolling resistance. Athletes can be trained better because there is more knowledge about muscle use.… (more)

Subjects/Keywords: sports; wheelchair; effectivity; propulsion

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APA (6th Edition):

Van der Ham, B. (2015). Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:6a20cd5b-3517-488b-bd46-663c12c4aa37

Chicago Manual of Style (16th Edition):

Van der Ham, B. “Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :.” 2015. Masters Thesis, Delft University of Technology. Accessed October 15, 2019. http://resolver.tudelft.nl/uuid:6a20cd5b-3517-488b-bd46-663c12c4aa37.

MLA Handbook (7th Edition):

Van der Ham, B. “Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :.” 2015. Web. 15 Oct 2019.

Vancouver:

Van der Ham B. Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 15]. Available from: http://resolver.tudelft.nl/uuid:6a20cd5b-3517-488b-bd46-663c12c4aa37.

Council of Science Editors:

Van der Ham B. Improving the effectivity of force translation from hand to push rim in sports wheelchairs: A redesign of the interface between push rim, hand and racket :. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:6a20cd5b-3517-488b-bd46-663c12c4aa37


Delft University of Technology

23. Krusharev, I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:.

Degree: 2015, Delft University of Technology

 The format and size specifications of the CubeSat platform require highly miniaturized subsystems, one of the most challenging ones being the propulsion system. Up to… (more)

Subjects/Keywords: propulsion; CubeSat; DelFFi; satellite

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APA (6th Edition):

Krusharev, I. (2015). Micro - Thruster Development: Propulsion System for the DelFFi Mission:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69

Chicago Manual of Style (16th Edition):

Krusharev, I. “Micro - Thruster Development: Propulsion System for the DelFFi Mission:.” 2015. Masters Thesis, Delft University of Technology. Accessed October 15, 2019. http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69.

MLA Handbook (7th Edition):

Krusharev, I. “Micro - Thruster Development: Propulsion System for the DelFFi Mission:.” 2015. Web. 15 Oct 2019.

Vancouver:

Krusharev I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 15]. Available from: http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69.

Council of Science Editors:

Krusharev I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69


University of Illinois – Urbana-Champaign

24. 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 October 15, 2019. 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. 15 Oct 2019.

Vancouver:

Patterson AP. System identification for development of distributed electric propulsion vertical take-off vehicles. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2019 Oct 15]. 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

25. 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 October 15, 2019. http://hdl.handle.net/2142/100997.

MLA Handbook (7th Edition):

Ahern, Drew. “Investigation of a space propulsion concept using inertial electrostatic confinement.” 2018. Web. 15 Oct 2019.

Vancouver:

Ahern D. Investigation of a space propulsion concept using inertial electrostatic confinement. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2018. [cited 2019 Oct 15]. 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

26. 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 October 15, 2019. 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. 15 Oct 2019.

Vancouver:

Asif M. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Oct 15]. 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


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 October 15, 2019. https://etda.libraries.psu.edu/catalog/15676suh301.

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

MLA Handbook (7th Edition):

Hsieh, Sang. “LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Web. 15 Oct 2019.

Vancouver:

Hsieh S. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Oct 15]. 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 Adelaide

28. Chadwick, Ashley Robert. Performance of Alternative Propellants in an Inductive Electric Propulsion System.

Degree: 2017, University of Adelaide

 Spacecraft fitted with electric propulsion systems can achieve a greater final velocity than chemical rockets, thus facilitating a range of new trajectories and exploratory mission… (more)

Subjects/Keywords: Electric propulsion; space; plasma

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APA (6th Edition):

Chadwick, A. R. (2017). Performance of Alternative Propellants in an Inductive Electric Propulsion System. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/119192

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):

Chadwick, Ashley Robert. “Performance of Alternative Propellants in an Inductive Electric Propulsion System.” 2017. Thesis, University of Adelaide. Accessed October 15, 2019. http://hdl.handle.net/2440/119192.

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

MLA Handbook (7th Edition):

Chadwick, Ashley Robert. “Performance of Alternative Propellants in an Inductive Electric Propulsion System.” 2017. Web. 15 Oct 2019.

Vancouver:

Chadwick AR. Performance of Alternative Propellants in an Inductive Electric Propulsion System. [Internet] [Thesis]. University of Adelaide; 2017. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/2440/119192.

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

Council of Science Editors:

Chadwick AR. Performance of Alternative Propellants in an Inductive Electric Propulsion System. [Thesis]. University of Adelaide; 2017. Available from: http://hdl.handle.net/2440/119192

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


University of Toronto

29. Spina, Robert. Development of an Electrothermal Propulsion System to Deorbit Small Satellites.

Degree: 2017, University of Toronto

The DAUNTLESS bus propulsion system, using carbon dioxide as the propellant, provides the capability to deorbit a satellite at the end of its mission. Large… (more)

Subjects/Keywords: Deorbit; Propulsion; Satellite; Space; 0538

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

APA (6th Edition):

Spina, R. (2017). Development of an Electrothermal Propulsion System to Deorbit Small Satellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79556

Chicago Manual of Style (16th Edition):

Spina, Robert. “Development of an Electrothermal Propulsion System to Deorbit Small Satellites.” 2017. Masters Thesis, University of Toronto. Accessed October 15, 2019. http://hdl.handle.net/1807/79556.

MLA Handbook (7th Edition):

Spina, Robert. “Development of an Electrothermal Propulsion System to Deorbit Small Satellites.” 2017. Web. 15 Oct 2019.

Vancouver:

Spina R. Development of an Electrothermal Propulsion System to Deorbit Small Satellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/1807/79556.

Council of Science Editors:

Spina R. Development of an Electrothermal Propulsion System to Deorbit Small Satellites. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79556


Virginia Tech

30. Webster III, John Ackroyd. Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling.

Degree: PhD, Aerospace and Ocean Engineering, 2019, Virginia Tech

 Small-scale marine propellers operate at low Reynolds numbers, where laminar-turbulent transition of the boundary layer can impact the distributions of pressure and shear stress on… (more)

Subjects/Keywords: Marine Propulsion; Transition Modeling; Hydrodynamics

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

APA (6th Edition):

Webster III, J. A. (2019). Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/93038

Chicago Manual of Style (16th Edition):

Webster III, John Ackroyd. “Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling.” 2019. Doctoral Dissertation, Virginia Tech. Accessed October 15, 2019. http://hdl.handle.net/10919/93038.

MLA Handbook (7th Edition):

Webster III, John Ackroyd. “Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling.” 2019. Web. 15 Oct 2019.

Vancouver:

Webster III JA. Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2019 Oct 15]. Available from: http://hdl.handle.net/10919/93038.

Council of Science Editors:

Webster III JA. Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/93038

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