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You searched for subject:(Propulsion). Showing records 1 – 30 of 996 total matches.

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Penn State University

1. Ho, Chien Hsiu. INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW.

Degree: 2020, Penn State University

 Beamed-energy propulsion provides a possible advanced propulsion method for Earth-launch systems with high-specific-impulse electric thrust and high payload mass fraction. The concept behind beamed-energy propulsion(more)

Subjects/Keywords: Propulsion; Beamed Energy Propulsion; Plasma

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APA (6th Edition):

Ho, C. H. (2020). INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/18010cbh5281

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

Chicago Manual of Style (16th Edition):

Ho, Chien Hsiu. “INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW.” 2020. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/18010cbh5281.

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

MLA Handbook (7th Edition):

Ho, Chien Hsiu. “INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW.” 2020. Web. 30 Sep 2020.

Vancouver:

Ho CH. INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW. [Internet] [Thesis]. Penn State University; 2020. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/18010cbh5281.

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

Council of Science Editors:

Ho CH. INVESTGATION OF BEAMED-MICROWAVE PLASMA GENERATION IN SUPERSONIC FLOW. [Thesis]. Penn State University; 2020. Available from: https://submit-etda.libraries.psu.edu/catalog/18010cbh5281

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

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 September 30, 2020. 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. 30 Sep 2020.

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 2020 Sep 30]. 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


Colorado State University

3. Andreano, Thomas Malachi. Performance and plume characterization of a laboratory krypton Hall thruster.

Degree: MS(M.S.), Mechanical Engineering, 2020, Colorado State University

 Hall thruster research has been in progress at the CSU Electric Propulsion and Plasma Engineering (CEPPE) lab for the past decade, however, a full performance… (more)

Subjects/Keywords: Hall thruster; propulsion; electric propulsion; space; plasma

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APA (6th Edition):

Andreano, T. M. (2020). Performance and plume characterization of a laboratory krypton Hall thruster. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/208509

Chicago Manual of Style (16th Edition):

Andreano, Thomas Malachi. “Performance and plume characterization of a laboratory krypton Hall thruster.” 2020. Masters Thesis, Colorado State University. Accessed September 30, 2020. http://hdl.handle.net/10217/208509.

MLA Handbook (7th Edition):

Andreano, Thomas Malachi. “Performance and plume characterization of a laboratory krypton Hall thruster.” 2020. Web. 30 Sep 2020.

Vancouver:

Andreano TM. Performance and plume characterization of a laboratory krypton Hall thruster. [Internet] [Masters thesis]. Colorado State University; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10217/208509.

Council of Science Editors:

Andreano TM. Performance and plume characterization of a laboratory krypton Hall thruster. [Masters Thesis]. Colorado State University; 2020. Available from: http://hdl.handle.net/10217/208509


Luleå University of Technology

4. 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 September 30, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-44228.

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

MLA Handbook (7th Edition):

Huarcaya, Victor. “Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System.” 2012. Web. 30 Sep 2020.

Vancouver:

Huarcaya V. Inertial Electrostatic Confinement Devices as an Advanced Electric Propulsion System. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2020 Sep 30]. 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

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

Degree: Docteur es, Mécanique des fluides, 2016, Université Paris-Saclay (ComUE)

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). Université Paris-Saclay (ComUE). 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, Université Paris-Saclay (ComUE). Accessed September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Du Pontavice E. Propulsion par cerf-volant : envol et pérégrinations : Kite propulsion : rise and wander. [Internet] [Doctoral dissertation]. Université Paris-Saclay (ComUE); 2016. [cited 2020 Sep 30]. 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]. Université Paris-Saclay (ComUE); 2016. Available from: http://www.theses.fr/2016SACLX015


University of Tennessee – Knoxville

6. 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 September 30, 2020. 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. 30 Sep 2020.

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 2020 Sep 30]. 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


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 September 30, 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. 30 Sep 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 Sep 30]. 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


Virginia Tech

8. DellaFera, Andrew Brian. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.

Degree: MS, Aerospace Engineering, 2019, Virginia Tech

 Ramjets and scramjets are the key to sustained flight at speeds above five times the speed of sound. These propulsion systems pose a challenging simulation… (more)

Subjects/Keywords: Hypersonic; Propulsion; Optimization

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APA (6th Edition):

DellaFera, A. B. (2019). Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95512

Chicago Manual of Style (16th Edition):

DellaFera, Andrew Brian. “Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.” 2019. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/95512.

MLA Handbook (7th Edition):

DellaFera, Andrew Brian. “Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.” 2019. Web. 30 Sep 2020.

Vancouver:

DellaFera AB. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. [Internet] [Masters thesis]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/95512.

Council of Science Editors:

DellaFera AB. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. [Masters Thesis]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/95512


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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Boronowsky KM. Non-homogeneous Hybrid Rocket Fuel for Enhanced Regression Rates Utilizing Partial Entrainment. [Internet] [Masters thesis]. San Jose State University; 2011. [cited 2020 Sep 30]. 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


Delft University of Technology

10. Wijnans, A.S. (author). 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 (author). “Electrodynamic Tether Experiment onboard the Delfi-1 Satellite.” 2012. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:437869ae-2a7d-40aa-b809-67b314dc91a7.

MLA Handbook (7th Edition):

Wijnans, A S (author). “Electrodynamic Tether Experiment onboard the Delfi-1 Satellite.” 2012. Web. 30 Sep 2020.

Vancouver:

Wijnans AS(. Electrodynamic Tether Experiment onboard the Delfi-1 Satellite. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Sep 30]. 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


Cal Poly

11. 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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2020 Sep 30]. 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


Colorado State University

12. Ham, Ryan K. Experimental investigation of heaterless hollow cathode ignition, An.

Degree: MS(M.S.), Mechanical Engineering, 2020, Colorado State University

 A hollow cathode is a specially designed plasma source that is capable of driving a large electron emission current throughout the course of a remarkably… (more)

Subjects/Keywords: plasma propulsion; satellite technology; thruster; propulsion; electric propulsion; space technology

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APA (6th Edition):

Ham, R. K. (2020). Experimental investigation of heaterless hollow cathode ignition, An. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/208490

Chicago Manual of Style (16th Edition):

Ham, Ryan K. “Experimental investigation of heaterless hollow cathode ignition, An.” 2020. Masters Thesis, Colorado State University. Accessed September 30, 2020. http://hdl.handle.net/10217/208490.

MLA Handbook (7th Edition):

Ham, Ryan K. “Experimental investigation of heaterless hollow cathode ignition, An.” 2020. Web. 30 Sep 2020.

Vancouver:

Ham RK. Experimental investigation of heaterless hollow cathode ignition, An. [Internet] [Masters thesis]. Colorado State University; 2020. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10217/208490.

Council of Science Editors:

Ham RK. Experimental investigation of heaterless hollow cathode ignition, An. [Masters Thesis]. Colorado State University; 2020. Available from: http://hdl.handle.net/10217/208490


Delft University of Technology

13. Pino, D.M. (author). Solar Concentrator Demonstrator for PocketQubes.

Degree: 2016, Delft University of Technology

Deployable systems for small satellites appear as an innovative solution to enhance the performance capabilities and enlarge the mission range of this category of spacecraft.… (more)

Subjects/Keywords: space propulsion; micro propulsion; PocketQube; solar thermal propulsion; inflatable; concentrator

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APA (6th Edition):

Pino, D. M. (. (2016). Solar Concentrator Demonstrator for PocketQubes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bc2146e6-fdaa-4be3-9e06-8e10a04362bf

Chicago Manual of Style (16th Edition):

Pino, D M (author). “Solar Concentrator Demonstrator for PocketQubes.” 2016. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:bc2146e6-fdaa-4be3-9e06-8e10a04362bf.

MLA Handbook (7th Edition):

Pino, D M (author). “Solar Concentrator Demonstrator for PocketQubes.” 2016. Web. 30 Sep 2020.

Vancouver:

Pino DM(. Solar Concentrator Demonstrator for PocketQubes. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:bc2146e6-fdaa-4be3-9e06-8e10a04362bf.

Council of Science Editors:

Pino DM(. Solar Concentrator Demonstrator for PocketQubes. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:bc2146e6-fdaa-4be3-9e06-8e10a04362bf


Cal Poly

14. 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 September 30, 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. 30 Sep 2020.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Sep 30]. Available from: https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93.

Council of Science Editors:

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


Penn State University

15. Mainwaring, Philip B. Design and Development of a K-Band Microwave Electrothermal Thruster.

Degree: 2016, Penn State University

 The microwave electrothermal thruster is an electric propulsion technology that has been under development at The Pennsylvania State University since the 1980s. Versions of this… (more)

Subjects/Keywords: microwave electrothermal thruster; electric propulsion; space propulsion; microwave plasma; plasma propulsion; resonant cavity

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

APA (6th Edition):

Mainwaring, P. B. (2016). Design and Development of a K-Band Microwave Electrothermal Thruster. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/8049g504g

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):

Mainwaring, Philip B. “Design and Development of a K-Band Microwave Electrothermal Thruster.” 2016. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/8049g504g.

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

MLA Handbook (7th Edition):

Mainwaring, Philip B. “Design and Development of a K-Band Microwave Electrothermal Thruster.” 2016. Web. 30 Sep 2020.

Vancouver:

Mainwaring PB. Design and Development of a K-Band Microwave Electrothermal Thruster. [Internet] [Thesis]. Penn State University; 2016. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/8049g504g.

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

Council of Science Editors:

Mainwaring PB. Design and Development of a K-Band Microwave Electrothermal Thruster. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/8049g504g

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


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 September 30, 2020. 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. 30 Sep 2020.

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 2020 Sep 30]. 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


Oregon State University

17. 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 September 30, 2020. http://hdl.handle.net/1957/51493.

MLA Handbook (7th Edition):

Lockwood, Raymond Marshall. “Pulsejet ejectors.” 1953. Web. 30 Sep 2020.

Vancouver:

Lockwood RM. Pulsejet ejectors. [Internet] [Masters thesis]. Oregon State University; 1953. [cited 2020 Sep 30]. 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


Texas A&M University

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

Degree: MS, Nuclear Engineering, 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. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649

Chicago Manual of Style (16th Edition):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Masters Thesis, Texas A&M University. Accessed September 30, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

MLA Handbook (7th Edition):

Appel, Bradley. “Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket.” 2012. Web. 30 Sep 2020.

Vancouver:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11649.

Council of Science Editors:

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


Penn State University

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

APA (6th Edition):

Asif, M. (2018). PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. (Thesis). Penn State University. Retrieved from https://submit-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 September 30, 2020. https://submit-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. 30 Sep 2020.

Vancouver:

Asif M. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2020 Sep 30]. Available from: https://submit-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://submit-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

20. Hsieh, Sang Chieh. 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. C. (2018). LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. (Thesis). Penn State University. Retrieved from https://submit-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 Chieh. “LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Thesis, Penn State University. Accessed September 30, 2020. https://submit-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 Chieh. “LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER.” 2018. Web. 30 Sep 2020.

Vancouver:

Hsieh SC. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2020 Sep 30]. Available from: https://submit-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 SC. LIFE ASSESSMENT OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Thesis]. Penn State University; 2018. Available from: https://submit-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


Penn State University

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

Degree: 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 . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11880

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):

Hopkins, Jeffrey Robert. “DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER .” 2011. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/11880.

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

MLA Handbook (7th Edition):

Hopkins, Jeffrey Robert. “DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER .” 2011. Web. 30 Sep 2020.

Vancouver:

Hopkins JR. DESIGN OPTIMIZATION AND DIRECT THRUST MEASUREMENT OF AN 8-GHz MICROWAVE ELECTROTHERMAL THRUSTER . [Internet] [Thesis]. Penn State University; 2011. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/11880.

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

Council of Science Editors:

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

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


Oregon State University

22. 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 September 30, 2020. 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. 30 Sep 2020.

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 2020 Sep 30]. 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

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

Degree: PhD, Aerospace Engineering, 2019, Virginia Tech

 Small-scale marine propellers exhibit transition from laminar to turbulent flow in the region near the surface of the blades. Regions of laminar and turbulent flow… (more)

Subjects/Keywords: Marine Propulsion; Transition Modeling; Hydrodynamics

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APA (6th Edition):

Webster, J. A. I. (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, John Ackroyd III. “Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling.” 2019. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/93038.

MLA Handbook (7th Edition):

Webster, John Ackroyd III. “Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling.” 2019. Web. 30 Sep 2020.

Vancouver:

Webster JAI. Design and Analysis of Low Reynolds Number Marine Propellers with Computational Fluid Dynamics (CFD) Transition Modeling. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/93038.

Council of Science Editors:

Webster JAI. 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


Embry-Riddle Aeronautical University

24. 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 https://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 September 30, 2020. https://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. 30 Sep 2020.

Vancouver:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Sep 30]. Available from: https://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: https://commons.erau.edu/edt/158

25. 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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Shimauchi T. Piston ring lubrication analysed by a unified hydrodynamic theory of thrust bearings. [Internet] [Doctoral dissertation]. Imperial College London; 1980. [cited 2020 Sep 30]. 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


Coventry University

26. 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 September 30, 2020. 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. 30 Sep 2020.

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 2020 Sep 30]. 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


Princeton University

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

Degree: PhD, 2017, Princeton University

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Feldman, Matthew Solomon. “The Direct Wave-Drive Thruster .” 2017. Doctoral Dissertation, Princeton University. Accessed September 30, 2020. http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k.

MLA Handbook (7th Edition):

Feldman, Matthew Solomon. “The Direct Wave-Drive Thruster .” 2017. Web. 30 Sep 2020.

Vancouver:

Feldman MS. The Direct Wave-Drive Thruster . [Internet] [Doctoral dissertation]. Princeton University; 2017. [cited 2020 Sep 30]. Available from: http://arks.princeton.edu/ark:/88435/dsp01kd17cw46k.

Council of Science Editors:

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


University of Toronto

28. 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 (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 September 30, 2020. http://hdl.handle.net/1807/79556.

MLA Handbook (7th Edition):

Spina, Robert. “Development of an Electrothermal Propulsion System to Deorbit Small Satellites.” 2017. Web. 30 Sep 2020.

Vancouver:

Spina R. Development of an Electrothermal Propulsion System to Deorbit Small Satellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2020 Sep 30]. 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


San Jose State University

29. Colleluori, Marco. Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3.

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

  After travelling through space dormant for 27 years, hopes were high for the reactivation of the hydrazine propulsion system on the International Sun Earth… (more)

Subjects/Keywords: Failure; Hydrazine; ISEE-3; Propulsion

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

APA (6th Edition):

Colleluori, M. (2015). Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.c8ba-c2kk ; https://scholarworks.sjsu.edu/etd_theses/4534

Chicago Manual of Style (16th Edition):

Colleluori, Marco. “Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3.” 2015. Masters Thesis, San Jose State University. Accessed September 30, 2020. https://doi.org/10.31979/etd.c8ba-c2kk ; https://scholarworks.sjsu.edu/etd_theses/4534.

MLA Handbook (7th Edition):

Colleluori, Marco. “Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3.” 2015. Web. 30 Sep 2020.

Vancouver:

Colleluori M. Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3. [Internet] [Masters thesis]. San Jose State University; 2015. [cited 2020 Sep 30]. Available from: https://doi.org/10.31979/etd.c8ba-c2kk ; https://scholarworks.sjsu.edu/etd_theses/4534.

Council of Science Editors:

Colleluori M. Characterization of the Performance and Failure Mechanisms of the Hydrazine Propulsion System of ISEE-3. [Masters Thesis]. San Jose State University; 2015. Available from: https://doi.org/10.31979/etd.c8ba-c2kk ; https://scholarworks.sjsu.edu/etd_theses/4534


Luleå University of Technology

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

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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Carlsvärd F. Experimental Test Rig Design and Testing of a Box-Bladed Propeller. [Internet] [Thesis]. Luleå University of Technology; 2013. [cited 2020 Sep 30]. 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

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