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You searched for subject:(developement of rocket engines). Showing records 1 – 30 of 255003 total matches.

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Brno University of Technology

1. Marcinko, Peter. Vývoj raketových motorů: Development of rocket engines.

Degree: 2019, Brno University of Technology

 This thesis describes the development of rocket engines since the beginning to present time. The thesis is divided into three parts. The first describes the… (more)

Subjects/Keywords: Raketový motor; raketa; technické parametre; vývoj raketových motorov; raketový program; Rocket engine; rocket; technical parameters; developement of rocket engines; rocket programe

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APA (6th Edition):

Marcinko, P. (2019). Vývoj raketových motorů: Development of rocket engines. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33320

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):

Marcinko, Peter. “Vývoj raketových motorů: Development of rocket engines.” 2019. Thesis, Brno University of Technology. Accessed February 28, 2021. http://hdl.handle.net/11012/33320.

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

MLA Handbook (7th Edition):

Marcinko, Peter. “Vývoj raketových motorů: Development of rocket engines.” 2019. Web. 28 Feb 2021.

Vancouver:

Marcinko P. Vývoj raketových motorů: Development of rocket engines. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/11012/33320.

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

Council of Science Editors:

Marcinko P. Vývoj raketových motorů: Development of rocket engines. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/33320

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


Brno University of Technology

2. Marcinko, Peter. Vývoj raketových motorů: Development of rocket engines.

Degree: 2014, Brno University of Technology

 This thesis describes the development of rocket engines since the beginning to present time. The thesis is divided into three parts. The first describes the… (more)

Subjects/Keywords: Raketový motor; raketa; technické parametre; vývoj raketových motorov; raketový program; Rocket engine; rocket; technical parameters; developement of rocket engines; rocket programe

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APA (6th Edition):

Marcinko, P. (2014). Vývoj raketových motorů: Development of rocket engines. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27145

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):

Marcinko, Peter. “Vývoj raketových motorů: Development of rocket engines.” 2014. Thesis, Brno University of Technology. Accessed February 28, 2021. http://hdl.handle.net/11012/27145.

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

MLA Handbook (7th Edition):

Marcinko, Peter. “Vývoj raketových motorů: Development of rocket engines.” 2014. Web. 28 Feb 2021.

Vancouver:

Marcinko P. Vývoj raketových motorů: Development of rocket engines. [Internet] [Thesis]. Brno University of Technology; 2014. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/11012/27145.

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

Council of Science Editors:

Marcinko P. Vývoj raketových motorů: Development of rocket engines. [Thesis]. Brno University of Technology; 2014. Available from: http://hdl.handle.net/11012/27145

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


Ryerson University

3. Lu, Zhiliu. Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors.

Degree: 2017, Ryerson University

 Hybrid rocket engines (HREs) are a chemical propulsion system that nominally combine the advantages of liquid-propellant rocket engines (LREs) and solid-propellant rocket motors (SRMs). HREs… (more)

Subjects/Keywords: Rocket engines  – Combustion  – Mathematical models; Rocket engines  – Thrust  – Mathematical models; Ballistics; Rocket engines

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APA (6th Edition):

Lu, Z. (2017). Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A7274

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):

Lu, Zhiliu. “Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors.” 2017. Thesis, Ryerson University. Accessed February 28, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A7274.

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

MLA Handbook (7th Edition):

Lu, Zhiliu. “Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors.” 2017. Web. 28 Feb 2021.

Vancouver:

Lu Z. Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors. [Internet] [Thesis]. Ryerson University; 2017. [cited 2021 Feb 28]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A7274.

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

Council of Science Editors:

Lu Z. Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A7274

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


Ryerson University

4. Velliaris, Alexander. Scale effects on hybrid rocket engine performance.

Degree: 2017, Ryerson University

 In the current study, the effects of scaling up a hybrid rocket engine (HRE) in size has on its performance is investigated. A HRE design… (more)

Subjects/Keywords: Rocket engines  – Thrust  – Mathematical models; Rocket engines  – Combustion  – Mathematical models; Rocket engines  – Propulsion systems; Rocket engines  – Design and construction

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APA (6th Edition):

Velliaris, A. (2017). Scale effects on hybrid rocket engine performance. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6782

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):

Velliaris, Alexander. “Scale effects on hybrid rocket engine performance.” 2017. Thesis, Ryerson University. Accessed February 28, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A6782.

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

MLA Handbook (7th Edition):

Velliaris, Alexander. “Scale effects on hybrid rocket engine performance.” 2017. Web. 28 Feb 2021.

Vancouver:

Velliaris A. Scale effects on hybrid rocket engine performance. [Internet] [Thesis]. Ryerson University; 2017. [cited 2021 Feb 28]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6782.

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

Council of Science Editors:

Velliaris A. Scale effects on hybrid rocket engine performance. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6782

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


Ryerson University

5. Wozney, Clayton Edward. Comparison Of Solid Rocket Motor Thrust Modulation Technique.

Degree: 2017, Ryerson University

 The thrust profiles of solid rocket motors are usually determined ahead of time by propellant composition and grain design. Traditional techniques for active thrust modulation… (more)

Subjects/Keywords: Rocket engines  – Combustion; Solid propellant rockets  – Combustion; Rocket engines  – Thrust

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APA (6th Edition):

Wozney, C. E. (2017). Comparison Of Solid Rocket Motor Thrust Modulation Technique. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6888

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):

Wozney, Clayton Edward. “Comparison Of Solid Rocket Motor Thrust Modulation Technique.” 2017. Thesis, Ryerson University. Accessed February 28, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A6888.

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

MLA Handbook (7th Edition):

Wozney, Clayton Edward. “Comparison Of Solid Rocket Motor Thrust Modulation Technique.” 2017. Web. 28 Feb 2021.

Vancouver:

Wozney CE. Comparison Of Solid Rocket Motor Thrust Modulation Technique. [Internet] [Thesis]. Ryerson University; 2017. [cited 2021 Feb 28]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6888.

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

Council of Science Editors:

Wozney CE. Comparison Of Solid Rocket Motor Thrust Modulation Technique. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6888

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


Oregon State University

6. Schmitz, Bruce Wayne. An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles.

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

Subjects/Keywords: Airplanes  – Rocket engines

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APA (6th Edition):

Schmitz, B. W. (1959). An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/50383

Chicago Manual of Style (16th Edition):

Schmitz, Bruce Wayne. “An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles.” 1959. Masters Thesis, Oregon State University. Accessed February 28, 2021. http://hdl.handle.net/1957/50383.

MLA Handbook (7th Edition):

Schmitz, Bruce Wayne. “An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles.” 1959. Web. 28 Feb 2021.

Vancouver:

Schmitz BW. An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles. [Internet] [Masters thesis]. Oregon State University; 1959. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1957/50383.

Council of Science Editors:

Schmitz BW. An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles. [Masters Thesis]. Oregon State University; 1959. Available from: http://hdl.handle.net/1957/50383


Texas Tech University

7. Grimes, Montgomery Dean. Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet.

Degree: 1990, Texas Tech University

 The power supply, used in this experiment, was designed from the start as a power source for a laboratory arcjet experiment. Therefore, it was never… (more)

Subjects/Keywords: Arcjet rocket engines

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APA (6th Edition):

Grimes, M. D. (1990). Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet. (Thesis). Texas Tech University. Retrieved from http://hdl.handle.net/2346/11798

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):

Grimes, Montgomery Dean. “Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet.” 1990. Thesis, Texas Tech University. Accessed February 28, 2021. http://hdl.handle.net/2346/11798.

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

MLA Handbook (7th Edition):

Grimes, Montgomery Dean. “Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet.” 1990. Web. 28 Feb 2021.

Vancouver:

Grimes MD. Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet. [Internet] [Thesis]. Texas Tech University; 1990. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/2346/11798.

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

Council of Science Editors:

Grimes MD. Design and construction of a multimode, regulated power supply for use on a 30 kilowatt arcjet. [Thesis]. Texas Tech University; 1990. Available from: http://hdl.handle.net/2346/11798

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


University of Arizona

8. Sekhon, Kalwant Singh, 1938-. Thrust vectoring experiments with gas injection .

Degree: 1964, University of Arizona

Subjects/Keywords: Rocket engines  – Thrust.

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APA (6th Edition):

Sekhon, Kalwant Singh, 1. (1964). Thrust vectoring experiments with gas injection . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/319830

Chicago Manual of Style (16th Edition):

Sekhon, Kalwant Singh, 1938-. “Thrust vectoring experiments with gas injection .” 1964. Masters Thesis, University of Arizona. Accessed February 28, 2021. http://hdl.handle.net/10150/319830.

MLA Handbook (7th Edition):

Sekhon, Kalwant Singh, 1938-. “Thrust vectoring experiments with gas injection .” 1964. Web. 28 Feb 2021.

Vancouver:

Sekhon, Kalwant Singh 1. Thrust vectoring experiments with gas injection . [Internet] [Masters thesis]. University of Arizona; 1964. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10150/319830.

Council of Science Editors:

Sekhon, Kalwant Singh 1. Thrust vectoring experiments with gas injection . [Masters Thesis]. University of Arizona; 1964. Available from: http://hdl.handle.net/10150/319830


Brno University of Technology

9. Říha, Jaroslav. Historie motorů BMW: History of BMW engines.

Degree: 2019, Brno University of Technology

 This bachelor thesis deals with the foundantion of the company BMW in Munich, the development of air, motorcycle and car engines, from their beginning to… (more)

Subjects/Keywords: Historický přehled vývoje; BMW; technická specifikace motorů; výkonnostní parametry.; Historical view of the developement; BMW; technical specifications of the engines; performance parameters.

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APA (6th Edition):

Říha, J. (2019). Historie motorů BMW: History of BMW engines. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/6250

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):

Říha, Jaroslav. “Historie motorů BMW: History of BMW engines.” 2019. Thesis, Brno University of Technology. Accessed February 28, 2021. http://hdl.handle.net/11012/6250.

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

MLA Handbook (7th Edition):

Říha, Jaroslav. “Historie motorů BMW: History of BMW engines.” 2019. Web. 28 Feb 2021.

Vancouver:

Říha J. Historie motorů BMW: History of BMW engines. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/11012/6250.

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

Council of Science Editors:

Říha J. Historie motorů BMW: History of BMW engines. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/6250

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


Brno University of Technology

10. Kříž, Tomáš. Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres.

Degree: 2019, Brno University of Technology

 Aim of this bachelor thesis is to describe current knowledge of hybrid rocket propulsion. Thesis describes the development of hybrid rocket engine, including its precise… (more)

Subjects/Keywords: Hybridní raketové motory (HRM); vesmírné manévry; paliva pro hybridní motory; okysličovadla pro hybridní motory; parametry raketových motorů; srovnání HRM s tradičními; vývoj HRM.; Hybrid rocket engines (HRE); space manoeuvres; propellants for hybrid engines; oxidizers for hybrid engines; parameters of hybrid engines; development of HRE.

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APA (6th Edition):

Kříž, T. (2019). Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/176633

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):

Kříž, Tomáš. “Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres.” 2019. Thesis, Brno University of Technology. Accessed February 28, 2021. http://hdl.handle.net/11012/176633.

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

MLA Handbook (7th Edition):

Kříž, Tomáš. “Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres.” 2019. Web. 28 Feb 2021.

Vancouver:

Kříž T. Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/11012/176633.

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

Council of Science Editors:

Kříž T. Hybridní raketové motory pro přesné provedení vesmírných manévrů: Throttleable hybrid rocket engines for precise aerospace manoeuvres. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/176633

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


Ryerson University

11. Baczynski, Christopher. Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor.

Degree: 2008, Ryerson University

 A comprehensive numerical model for internal ballistic simulation under dynamic flow, combustion and structural vibration conditions is used to investigate the effectiveness of grain port… (more)

Subjects/Keywords: Rocket engines  – Combustion  – Mathematical models; Rocket engines  – Combustion; Rocket engines  – Design and construction

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APA (6th Edition):

Baczynski, C. (2008). Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1697

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):

Baczynski, Christopher. “Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor.” 2008. Thesis, Ryerson University. Accessed February 28, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1697.

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

MLA Handbook (7th Edition):

Baczynski, Christopher. “Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor.” 2008. Web. 28 Feb 2021.

Vancouver:

Baczynski C. Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor. [Internet] [Thesis]. Ryerson University; 2008. [cited 2021 Feb 28]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1697.

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

Council of Science Editors:

Baczynski C. Effects Of Grain Geometry And Vibration On The Suppression Of Combustion Instability In A Solid Rocket Motor. [Thesis]. Ryerson University; 2008. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1697

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


Georgia Tech

12. Lioi, Christopher. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 This thesis concerns the consistent linear acoustic stability analysis of an engine modeled on the RD-170, a prototypical example of an Oxidizer Rich Staged Combustion… (more)

Subjects/Keywords: Combustion instabilities; Acoustics; Liquid rocket engines; ORSC engines; Finite element analysis; LES; Flame transfer function

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APA (6th Edition):

Lioi, C. (2019). Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62579

Chicago Manual of Style (16th Edition):

Lioi, Christopher. “Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.” 2019. Doctoral Dissertation, Georgia Tech. Accessed February 28, 2021. http://hdl.handle.net/1853/62579.

MLA Handbook (7th Edition):

Lioi, Christopher. “Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.” 2019. Web. 28 Feb 2021.

Vancouver:

Lioi C. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1853/62579.

Council of Science Editors:

Lioi C. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62579


Ryerson University

13. Wongyai, Potchara. Fuel regression rate estimation model for swirling-flow hybrid rocket engines.

Degree: 2015, Ryerson University

 In the current study, an analytical model to estimate the fuel surface regression rate of hybrid rocket engines with head-end swirling flow oxidizer injection is… (more)

Subjects/Keywords: Rocket engines  – Fluid dynamics.; Fluid mechanics.; Propulsion systems  – Mathematical models.

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APA (6th Edition):

Wongyai, P. (2015). Fuel regression rate estimation model for swirling-flow hybrid rocket engines. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A3644

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):

Wongyai, Potchara. “Fuel regression rate estimation model for swirling-flow hybrid rocket engines.” 2015. Thesis, Ryerson University. Accessed February 28, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A3644.

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

MLA Handbook (7th Edition):

Wongyai, Potchara. “Fuel regression rate estimation model for swirling-flow hybrid rocket engines.” 2015. Web. 28 Feb 2021.

Vancouver:

Wongyai P. Fuel regression rate estimation model for swirling-flow hybrid rocket engines. [Internet] [Thesis]. Ryerson University; 2015. [cited 2021 Feb 28]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3644.

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

Council of Science Editors:

Wongyai P. Fuel regression rate estimation model for swirling-flow hybrid rocket engines. [Thesis]. Ryerson University; 2015. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3644

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


Cranfield University

14. Tucker, J. A whole life assessment of extruded double base propellants.

Degree: PhD, 2013, Cranfield University

 The manufacturing process for solventless extruded double base propellants involves a number of rolling and reworking stages. Throughout these processes a decrease in weight average… (more)

Subjects/Keywords: Nitrocellulose; Double-based rocket propellants; Propulsion, engines and fuels

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APA (6th Edition):

Tucker, J. (2013). A whole life assessment of extruded double base propellants. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/8032

Chicago Manual of Style (16th Edition):

Tucker, J. “A whole life assessment of extruded double base propellants.” 2013. Doctoral Dissertation, Cranfield University. Accessed February 28, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/8032.

MLA Handbook (7th Edition):

Tucker, J. “A whole life assessment of extruded double base propellants.” 2013. Web. 28 Feb 2021.

Vancouver:

Tucker J. A whole life assessment of extruded double base propellants. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2021 Feb 28]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8032.

Council of Science Editors:

Tucker J. A whole life assessment of extruded double base propellants. [Doctoral Dissertation]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8032


Cranfield University

15. Tucker, J. A whole life assessment of extruded double base propellants.

Degree: PhD, 2013, Cranfield University

 The manufacturing process for solventless extruded double base propellants involves a number of rolling and reworking stages. Throughout these processes a decrease in weight average… (more)

Subjects/Keywords: 662; Nitrocellulose; Double-based rocket propellants; Propulsion, engines and fuels

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APA (6th Edition):

Tucker, J. (2013). A whole life assessment of extruded double base propellants. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/8032 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.578041

Chicago Manual of Style (16th Edition):

Tucker, J. “A whole life assessment of extruded double base propellants.” 2013. Doctoral Dissertation, Cranfield University. Accessed February 28, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/8032 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.578041.

MLA Handbook (7th Edition):

Tucker, J. “A whole life assessment of extruded double base propellants.” 2013. Web. 28 Feb 2021.

Vancouver:

Tucker J. A whole life assessment of extruded double base propellants. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2021 Feb 28]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8032 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.578041.

Council of Science Editors:

Tucker J. A whole life assessment of extruded double base propellants. [Doctoral Dissertation]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8032 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.578041

16. Arunachalam, Swaminath Adi. The drag resistance of burning drops.

Degree: PhD, 1965, Imperial College London

 An experimental study has been made of the drag resistance of burning drops. Distance-time records of single freely falling drops of iso-pentane n-heptane and benzene,… (more)

Subjects/Keywords: 629.134; Rocket engines, Combustion

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APA (6th Edition):

Arunachalam, S. A. (1965). The drag resistance of burning drops. (Doctoral Dissertation). Imperial College London. Retrieved from http://hdl.handle.net/10044/1/16980

Chicago Manual of Style (16th Edition):

Arunachalam, Swaminath Adi. “The drag resistance of burning drops.” 1965. Doctoral Dissertation, Imperial College London. Accessed February 28, 2021. http://hdl.handle.net/10044/1/16980.

MLA Handbook (7th Edition):

Arunachalam, Swaminath Adi. “The drag resistance of burning drops.” 1965. Web. 28 Feb 2021.

Vancouver:

Arunachalam SA. The drag resistance of burning drops. [Internet] [Doctoral dissertation]. Imperial College London; 1965. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10044/1/16980.

Council of Science Editors:

Arunachalam SA. The drag resistance of burning drops. [Doctoral Dissertation]. Imperial College London; 1965. Available from: http://hdl.handle.net/10044/1/16980


Kristianstad University

17. Alwandi, Roaa. From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone.

Degree: Kristianstad University, 2012, Kristianstad University

  This essay will exlopre the character of one of our times most beloved fictional characters, Harry Potter. The purpose of this esay is to… (more)

Subjects/Keywords: Harry Potter; Developement of character; characterisation analysis

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APA (6th Edition):

Alwandi, R. (2012). From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone. (Thesis). Kristianstad University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hkr:diva-10216

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):

Alwandi, Roaa. “From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone.” 2012. Thesis, Kristianstad University. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hkr:diva-10216.

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

MLA Handbook (7th Edition):

Alwandi, Roaa. “From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone.” 2012. Web. 28 Feb 2021.

Vancouver:

Alwandi R. From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone. [Internet] [Thesis]. Kristianstad University; 2012. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hkr:diva-10216.

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

Council of Science Editors:

Alwandi R. From "Abnormal" Orphan to Celebrated Hero: A discussion of Harry's development in J.K. Rowling's Harry Potter and the Philosopher's Stone. [Thesis]. Kristianstad University; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hkr:diva-10216

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


Indian Institute of Science

18. Biju Kumar, K S. Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine.

Degree: PhD, Faculty of Engineering, 2014, Indian Institute of Science

 Physical mechanism for high frequency instability in cryogenic engines at low hydrogen injection temperature has been a subject of debate for long time. Experimental and… (more)

Subjects/Keywords: Liquid Propellant Rocket; Cryogenic Rocket Engines; Combustion Instability; Cryogenic Engines - Combustion Instability; Hydrogen Injection Temperature Combustion Instability; Cryogenic Engines - Combustion Modeling; Combustion Instability; Heat Engineering

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APA (6th Edition):

Biju Kumar, K. S. (2014). Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2297

Chicago Manual of Style (16th Edition):

Biju Kumar, K S. “Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine.” 2014. Doctoral Dissertation, Indian Institute of Science. Accessed February 28, 2021. http://etd.iisc.ac.in/handle/2005/2297.

MLA Handbook (7th Edition):

Biju Kumar, K S. “Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine.” 2014. Web. 28 Feb 2021.

Vancouver:

Biju Kumar KS. Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2014. [cited 2021 Feb 28]. Available from: http://etd.iisc.ac.in/handle/2005/2297.

Council of Science Editors:

Biju Kumar KS. Role Of Hydrogen Injection Temperature On The Combustion Instability Of Cryogenic Rocket Engine. [Doctoral Dissertation]. Indian Institute of Science; 2014. Available from: http://etd.iisc.ac.in/handle/2005/2297


Georgia Tech

19. Wright, James Glynn. A study of clutches for use in a clutchoperated power screw actuator for space applications.

Degree: PhD, Mechanical engineering, 1968, Georgia Tech

Subjects/Keywords: Clutches (Machinery); Rocket engines Control systems

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APA (6th Edition):

Wright, J. G. (1968). A study of clutches for use in a clutchoperated power screw actuator for space applications. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/17399

Chicago Manual of Style (16th Edition):

Wright, James Glynn. “A study of clutches for use in a clutchoperated power screw actuator for space applications.” 1968. Doctoral Dissertation, Georgia Tech. Accessed February 28, 2021. http://hdl.handle.net/1853/17399.

MLA Handbook (7th Edition):

Wright, James Glynn. “A study of clutches for use in a clutchoperated power screw actuator for space applications.” 1968. Web. 28 Feb 2021.

Vancouver:

Wright JG. A study of clutches for use in a clutchoperated power screw actuator for space applications. [Internet] [Doctoral dissertation]. Georgia Tech; 1968. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1853/17399.

Council of Science Editors:

Wright JG. A study of clutches for use in a clutchoperated power screw actuator for space applications. [Doctoral Dissertation]. Georgia Tech; 1968. Available from: http://hdl.handle.net/1853/17399


Georgia Tech

20. Lores, Manuel Edward. A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines.

Degree: PhD, Aerospace Engineering, 1972, Georgia Tech

Subjects/Keywords: Rocket engines Combustion; Liquid propellant rockets

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APA (6th Edition):

Lores, M. E. (1972). A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12440

Chicago Manual of Style (16th Edition):

Lores, Manuel Edward. “A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines.” 1972. Doctoral Dissertation, Georgia Tech. Accessed February 28, 2021. http://hdl.handle.net/1853/12440.

MLA Handbook (7th Edition):

Lores, Manuel Edward. “A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines.” 1972. Web. 28 Feb 2021.

Vancouver:

Lores ME. A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines. [Internet] [Doctoral dissertation]. Georgia Tech; 1972. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1853/12440.

Council of Science Editors:

Lores ME. A theoretical study of nonlinear longitudinal combustion instability in liquid propellant rocket engines. [Doctoral Dissertation]. Georgia Tech; 1972. Available from: http://hdl.handle.net/1853/12440


Georgia Tech

21. Kooker, Douglas Edward. Numerical solution of axial-mode instability problems in solid propellant rocket motors.

Degree: PhD, Aerospace Engineering, 1973, Georgia Tech

Subjects/Keywords: Solid propellant rockets; Rocket engines Combustion

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APA (6th Edition):

Kooker, D. E. (1973). Numerical solution of axial-mode instability problems in solid propellant rocket motors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13066

Chicago Manual of Style (16th Edition):

Kooker, Douglas Edward. “Numerical solution of axial-mode instability problems in solid propellant rocket motors.” 1973. Doctoral Dissertation, Georgia Tech. Accessed February 28, 2021. http://hdl.handle.net/1853/13066.

MLA Handbook (7th Edition):

Kooker, Douglas Edward. “Numerical solution of axial-mode instability problems in solid propellant rocket motors.” 1973. Web. 28 Feb 2021.

Vancouver:

Kooker DE. Numerical solution of axial-mode instability problems in solid propellant rocket motors. [Internet] [Doctoral dissertation]. Georgia Tech; 1973. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1853/13066.

Council of Science Editors:

Kooker DE. Numerical solution of axial-mode instability problems in solid propellant rocket motors. [Doctoral Dissertation]. Georgia Tech; 1973. Available from: http://hdl.handle.net/1853/13066


Virginia Tech

22. Qian, Xin. Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor.

Degree: MS, Aerospace and Ocean Engineering, 1990, Virginia Tech

Subjects/Keywords: Rocket engines; LD5655.V855 1990.Q536

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APA (6th Edition):

Qian, X. (1990). Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41483

Chicago Manual of Style (16th Edition):

Qian, Xin. “Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor.” 1990. Masters Thesis, Virginia Tech. Accessed February 28, 2021. http://hdl.handle.net/10919/41483.

MLA Handbook (7th Edition):

Qian, Xin. “Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor.” 1990. Web. 28 Feb 2021.

Vancouver:

Qian X. Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor. [Internet] [Masters thesis]. Virginia Tech; 1990. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10919/41483.

Council of Science Editors:

Qian X. Flow field investigation in pulse 1 motor of a two-pulse solid rocket motor. [Masters Thesis]. Virginia Tech; 1990. Available from: http://hdl.handle.net/10919/41483


Virginia Tech

23. Hetreed, Christopher F. Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor.

Degree: MS, Aerospace Engineering, 1989, Virginia Tech

  Cold-flow tests were conducted in mediums of air and water to investigate the internal flow field about the nozzle region of a proposed solid… (more)

Subjects/Keywords: Rocket engines; LD5655.V855 1989.H479

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APA (6th Edition):

Hetreed, C. F. (1989). Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46038

Chicago Manual of Style (16th Edition):

Hetreed, Christopher F. “Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor.” 1989. Masters Thesis, Virginia Tech. Accessed February 28, 2021. http://hdl.handle.net/10919/46038.

MLA Handbook (7th Edition):

Hetreed, Christopher F. “Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor.” 1989. Web. 28 Feb 2021.

Vancouver:

Hetreed CF. Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor. [Internet] [Masters thesis]. Virginia Tech; 1989. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10919/46038.

Council of Science Editors:

Hetreed CF. Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor. [Masters Thesis]. Virginia Tech; 1989. Available from: http://hdl.handle.net/10919/46038


Virginia Tech

24. Lupi, Alessandro. CFD analysis and redesign of centrifugal impeller flows for rocket pumps.

Degree: MS, Mechanical Engineering, 1993, Virginia Tech

  The analysis and redesign of a centrifugal impeller for a rocket pump is presented in this thesis. A baseline impeller was designed by Rocketdyne… (more)

Subjects/Keywords: Rocket engines; LD5655.V855 1993.L875

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APA (6th Edition):

Lupi, A. (1993). CFD analysis and redesign of centrifugal impeller flows for rocket pumps. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43488

Chicago Manual of Style (16th Edition):

Lupi, Alessandro. “CFD analysis and redesign of centrifugal impeller flows for rocket pumps.” 1993. Masters Thesis, Virginia Tech. Accessed February 28, 2021. http://hdl.handle.net/10919/43488.

MLA Handbook (7th Edition):

Lupi, Alessandro. “CFD analysis and redesign of centrifugal impeller flows for rocket pumps.” 1993. Web. 28 Feb 2021.

Vancouver:

Lupi A. CFD analysis and redesign of centrifugal impeller flows for rocket pumps. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10919/43488.

Council of Science Editors:

Lupi A. CFD analysis and redesign of centrifugal impeller flows for rocket pumps. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/43488


Virginia Tech

25. Doan, Andrew W. 3-D flow and performance of a rocket pump inducer at design and off-design flow rates.

Degree: MS, Mechanical Engineering, 1994, Virginia Tech

see document Advisors/Committee Members: Moore, John (committeechair), Brown, Eugene F. (committee member), Dancey, Clinton L. (committee member).

Subjects/Keywords: Rocket engines; LD5655.V855 1994.D636

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APA (6th Edition):

Doan, A. W. (1994). 3-D flow and performance of a rocket pump inducer at design and off-design flow rates. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/46018

Chicago Manual of Style (16th Edition):

Doan, Andrew W. “3-D flow and performance of a rocket pump inducer at design and off-design flow rates.” 1994. Masters Thesis, Virginia Tech. Accessed February 28, 2021. http://hdl.handle.net/10919/46018.

MLA Handbook (7th Edition):

Doan, Andrew W. “3-D flow and performance of a rocket pump inducer at design and off-design flow rates.” 1994. Web. 28 Feb 2021.

Vancouver:

Doan AW. 3-D flow and performance of a rocket pump inducer at design and off-design flow rates. [Internet] [Masters thesis]. Virginia Tech; 1994. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10919/46018.

Council of Science Editors:

Doan AW. 3-D flow and performance of a rocket pump inducer at design and off-design flow rates. [Masters Thesis]. Virginia Tech; 1994. Available from: http://hdl.handle.net/10919/46018


Virginia Tech

26. Dwyer, Michael E. Quasi-optimal steady state and transient maneuvers with and without thrust vectoring.

Degree: MS, Aerospace Engineering, 1993, Virginia Tech

see document Advisors/Committee Members: Lutze, Frederick H. Jr. (committeechair), Cliff, Eugene M. (committee member), Durham, Wayne C. (committee member).

Subjects/Keywords: Rocket engines; LD5655.V855 1993.D893

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APA (6th Edition):

Dwyer, M. E. (1993). Quasi-optimal steady state and transient maneuvers with and without thrust vectoring. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44931

Chicago Manual of Style (16th Edition):

Dwyer, Michael E. “Quasi-optimal steady state and transient maneuvers with and without thrust vectoring.” 1993. Masters Thesis, Virginia Tech. Accessed February 28, 2021. http://hdl.handle.net/10919/44931.

MLA Handbook (7th Edition):

Dwyer, Michael E. “Quasi-optimal steady state and transient maneuvers with and without thrust vectoring.” 1993. Web. 28 Feb 2021.

Vancouver:

Dwyer ME. Quasi-optimal steady state and transient maneuvers with and without thrust vectoring. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10919/44931.

Council of Science Editors:

Dwyer ME. Quasi-optimal steady state and transient maneuvers with and without thrust vectoring. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/44931


University of KwaZulu-Natal

27. Sithole, Thando. Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province.

Degree: 2019, University of KwaZulu-Natal

 The National Development Plan (NDP) highlights the need for a capable and developmental state. This capable and developmental state will be enabled by, inter alia,… (more)

Subjects/Keywords: Monitoring evaluation of training; Developement training; Office of the Premier

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APA (6th Edition):

Sithole, T. (2019). Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province. (Thesis). University of KwaZulu-Natal. Retrieved from https://researchspace.ukzn.ac.za/handle/10413/17056

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):

Sithole, Thando. “Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province.” 2019. Thesis, University of KwaZulu-Natal. Accessed February 28, 2021. https://researchspace.ukzn.ac.za/handle/10413/17056.

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

MLA Handbook (7th Edition):

Sithole, Thando. “Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province.” 2019. Web. 28 Feb 2021.

Vancouver:

Sithole T. Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province. [Internet] [Thesis]. University of KwaZulu-Natal; 2019. [cited 2021 Feb 28]. Available from: https://researchspace.ukzn.ac.za/handle/10413/17056.

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

Council of Science Editors:

Sithole T. Monitoring and evaluation of training and development programmes within the office of the premier, KwaZulu-Natal province. [Thesis]. University of KwaZulu-Natal; 2019. Available from: https://researchspace.ukzn.ac.za/handle/10413/17056

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


Penn State University

28. 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://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 February 28, 2021. 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. 28 Feb 2021.

Vancouver:

Asif M. PROTOTYPING AND OPTIMIZATION OF A MINIATURE MICROWAVE-FREQUENCY ION THRUSTER. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Feb 28]. 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


Delft University of Technology

29. Wildvank, Roy (author). Launch vehicle structural mass prediction model.

Degree: 2018, Delft University of Technology

Accurate dry mass prediction is essential in early design phases of a launch system. To predict structural mass of a launch vehicle more accurate at… (more)

Subjects/Keywords: mass model; Launch Vehicle design; Launch Vehicle optimization; rocket structures; buckling of rocket structures

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APA (6th Edition):

Wildvank, R. (. (2018). Launch vehicle structural mass prediction model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bb943ec1-1a2a-462d-873e-05338b29235f

Chicago Manual of Style (16th Edition):

Wildvank, Roy (author). “Launch vehicle structural mass prediction model.” 2018. Masters Thesis, Delft University of Technology. Accessed February 28, 2021. http://resolver.tudelft.nl/uuid:bb943ec1-1a2a-462d-873e-05338b29235f.

MLA Handbook (7th Edition):

Wildvank, Roy (author). “Launch vehicle structural mass prediction model.” 2018. Web. 28 Feb 2021.

Vancouver:

Wildvank R(. Launch vehicle structural mass prediction model. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Feb 28]. Available from: http://resolver.tudelft.nl/uuid:bb943ec1-1a2a-462d-873e-05338b29235f.

Council of Science Editors:

Wildvank R(. Launch vehicle structural mass prediction model. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:bb943ec1-1a2a-462d-873e-05338b29235f

30. Perovšek, Jaka. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.

Degree: Electrical and Space Engineering, 2018, Luleå University of Technology

  A visualisation procedure was developed which predicts excited hydroxyl (OH*) radiation from the Computational Fluid Dynamics (CFD) solutions of cryogenic hydrogen-oxygen rocket flames. The… (more)

Subjects/Keywords: spectral modelling; excited hydroxyl radiation; OH* radiation; ray tracing; spectroscopy; rocket combustion chambers; rocket engines; hydrogen-oxygen combustion; combustion instabilities; Aerospace Engineering; Rymd- och flygteknik

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APA (6th Edition):

Perovšek, J. (2018). Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277

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):

Perovšek, Jaka. “Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.” 2018. Thesis, Luleå University of Technology. Accessed February 28, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277.

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

MLA Handbook (7th Edition):

Perovšek, Jaka. “Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.” 2018. Web. 28 Feb 2021.

Vancouver:

Perovšek J. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. [Internet] [Thesis]. Luleå University of Technology; 2018. [cited 2021 Feb 28]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277.

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

Council of Science Editors:

Perovšek J. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. [Thesis]. Luleå University of Technology; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277

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

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