Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(rocket). Showing records 1 – 30 of 406 total matches.

[1] [2] [3] [4] [5] … [14]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

Languages

Country

▼ Search Limiters


Kingston University

1. Karaveckas, Linas. Development of low-cost pressurisation system for rocket engines.

Degree: PhD, 2019, Kingston University

 Increasing demand for low-cost satellites requires new affordable launch vehicles. Rocket turbopump systems are deemed to be one of the most complex and expensive components… (more)

Subjects/Keywords: rocket piston pump; rocket pressurisation systems; rocket turbopump; rocket reciprocating pump; low-cost rocket pump

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Karaveckas, L. (2019). Development of low-cost pressurisation system for rocket engines. (Doctoral Dissertation). Kingston University. Retrieved from http://eprints.kingston.ac.uk/id/eprint/43962/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.789357

Chicago Manual of Style (16th Edition):

Karaveckas, Linas. “Development of low-cost pressurisation system for rocket engines.” 2019. Doctoral Dissertation, Kingston University. Accessed February 28, 2021. http://eprints.kingston.ac.uk/id/eprint/43962/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.789357.

MLA Handbook (7th Edition):

Karaveckas, Linas. “Development of low-cost pressurisation system for rocket engines.” 2019. Web. 28 Feb 2021.

Vancouver:

Karaveckas L. Development of low-cost pressurisation system for rocket engines. [Internet] [Doctoral dissertation]. Kingston University; 2019. [cited 2021 Feb 28]. Available from: http://eprints.kingston.ac.uk/id/eprint/43962/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.789357.

Council of Science Editors:

Karaveckas L. Development of low-cost pressurisation system for rocket engines. [Doctoral Dissertation]. Kingston University; 2019. Available from: http://eprints.kingston.ac.uk/id/eprint/43962/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.789357


University of KwaZulu-Natal

2. Balmogim, Udil. Design and development of the Phoenix-1B hybrid rocket.

Degree: 2017, University of KwaZulu-Natal

 In August 2014, South Africa’s first university-based hybrid rocket, Phoenix-1A, was launched at the Overberg Test Range near Cape Agulhas. The vehicle suffered nozzle and… (more)

Subjects/Keywords: Rocket design.; Rocket engine.; Hybrid rocket.; Pheonix-1B hybrid rocket.; Hybrid propultasion system.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Balmogim, U. (2017). Design and development of the Phoenix-1B hybrid rocket. (Thesis). University of KwaZulu-Natal. Retrieved from http://hdl.handle.net/10413/16062

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):

Balmogim, Udil. “Design and development of the Phoenix-1B hybrid rocket.” 2017. Thesis, University of KwaZulu-Natal. Accessed February 28, 2021. http://hdl.handle.net/10413/16062.

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

MLA Handbook (7th Edition):

Balmogim, Udil. “Design and development of the Phoenix-1B hybrid rocket.” 2017. Web. 28 Feb 2021.

Vancouver:

Balmogim U. Design and development of the Phoenix-1B hybrid rocket. [Internet] [Thesis]. University of KwaZulu-Natal; 2017. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/10413/16062.

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

Council of Science Editors:

Balmogim U. Design and development of the Phoenix-1B hybrid rocket. [Thesis]. University of KwaZulu-Natal; 2017. Available from: http://hdl.handle.net/10413/16062

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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


Mississippi State University

5. Patterson, William Ray. DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS.

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

 A rocket test system was developed and fabricated for the purpose of testing hybrid rocket motors. The test system includes a rocket test stand, load… (more)

Subjects/Keywords: hybrid; rocket

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Patterson, W. R. (2009). DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-07062009-120546/ ;

Chicago Manual of Style (16th Edition):

Patterson, William Ray. “DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS.” 2009. Masters Thesis, Mississippi State University. Accessed February 28, 2021. http://sun.library.msstate.edu/ETD-db/theses/available/etd-07062009-120546/ ;.

MLA Handbook (7th Edition):

Patterson, William Ray. “DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS.” 2009. Web. 28 Feb 2021.

Vancouver:

Patterson WR. DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS. [Internet] [Masters thesis]. Mississippi State University; 2009. [cited 2021 Feb 28]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07062009-120546/ ;.

Council of Science Editors:

Patterson WR. DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS. [Masters Thesis]. Mississippi State University; 2009. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07062009-120546/ ;


University of Kashmir

6. Arora, Amar Jit. Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;.

Degree: 2014, University of Kashmir

This thesis deals with the propellant chemistry has made an unprecedented progress in the last two decades The important topics in composite propellant research are… (more)

Subjects/Keywords: Rocket-Propellants; Phenol-Formaldehyde

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Arora, A. J. (2014). Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;. (Thesis). University of Kashmir. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/23982

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):

Arora, Amar Jit. “Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;.” 2014. Thesis, University of Kashmir. Accessed February 28, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/23982.

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

MLA Handbook (7th Edition):

Arora, Amar Jit. “Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;.” 2014. Web. 28 Feb 2021.

Vancouver:

Arora AJ. Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;. [Internet] [Thesis]. University of Kashmir; 2014. [cited 2021 Feb 28]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/23982.

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

Council of Science Editors:

Arora AJ. Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;. [Thesis]. University of Kashmir; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/23982

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


Texas A&M University

7. Thomas, James C. Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains.

Degree: MS, Mechanical Engineering, 2014, Texas A&M University

 Low regression rates in hybrid rockets limit their use and capability, but additive aluminum nano-particles represent a possible solution to this problem. In this thesis,… (more)

Subjects/Keywords: Hybrid; Rocket; HTPB; Aluminum; Regression

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Thomas, J. C. (2014). Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154244

Chicago Manual of Style (16th Edition):

Thomas, James C. “Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains.” 2014. Masters Thesis, Texas A&M University. Accessed February 28, 2021. http://hdl.handle.net/1969.1/154244.

MLA Handbook (7th Edition):

Thomas, James C. “Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains.” 2014. Web. 28 Feb 2021.

Vancouver:

Thomas JC. Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains. [Internet] [Masters thesis]. Texas A&M University; 2014. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1969.1/154244.

Council of Science Editors:

Thomas JC. Hybrid Rocket Burning Rate Enhancement by Nano-Scale Additives in HTPB Fuel Grains. [Masters Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154244


Texas A&M University

8. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 February 28, 2021. 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. 28 Feb 2021.

Vancouver:

Appel B. Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Feb 28]. 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


Delft University of Technology

9. Powell, S.J. (author). CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor.

Degree: 2015, Delft University of Technology

In this MSc thesis, a 4N Bi-Propellant rocket motor was designed using numerical analysis tools. Four motors were built and tested. The results are presented… (more)

Subjects/Keywords: Micro Bi-Propellant Rocket Motor

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Powell, S. J. (. (2015). CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6

Chicago Manual of Style (16th Edition):

Powell, S J (author). “CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor.” 2015. Masters Thesis, Delft University of Technology. Accessed February 28, 2021. http://resolver.tudelft.nl/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6.

MLA Handbook (7th Edition):

Powell, S J (author). “CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor.” 2015. Web. 28 Feb 2021.

Vancouver:

Powell SJ(. CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Feb 28]. Available from: http://resolver.tudelft.nl/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6.

Council of Science Editors:

Powell SJ(. CubeSatMicro-Propulsion: Design and Validation of a Micro Bi-Propellant Rocket Motor. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:a6de0cf0-a562-41e0-8b34-b53b839385d6


Delft University of Technology

10. Engelen, F.M. (author). Quantitative risk analysis of unguided rocket trajectories.

Degree: 2012, Delft University of Technology

 These days more and more rockets are developed by companies, students and other amateurs. To assess the safety of these rockets, a method is necessary… (more)

Subjects/Keywords: Rocket trajectory Stratos simulation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Engelen, F. M. (. (2012). Quantitative risk analysis of unguided rocket trajectories. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2dfae5a6-809e-484d-8b3e-ebd146d891f3

Chicago Manual of Style (16th Edition):

Engelen, F M (author). “Quantitative risk analysis of unguided rocket trajectories.” 2012. Masters Thesis, Delft University of Technology. Accessed February 28, 2021. http://resolver.tudelft.nl/uuid:2dfae5a6-809e-484d-8b3e-ebd146d891f3.

MLA Handbook (7th Edition):

Engelen, F M (author). “Quantitative risk analysis of unguided rocket trajectories.” 2012. Web. 28 Feb 2021.

Vancouver:

Engelen FM(. Quantitative risk analysis of unguided rocket trajectories. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Feb 28]. Available from: http://resolver.tudelft.nl/uuid:2dfae5a6-809e-484d-8b3e-ebd146d891f3.

Council of Science Editors:

Engelen FM(. Quantitative risk analysis of unguided rocket trajectories. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:2dfae5a6-809e-484d-8b3e-ebd146d891f3


Brno University of Technology

11. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

12. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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

13. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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


University of Adelaide

14. Hardi, Justin S. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.

Degree: 2012, University of Adelaide

 Self-sustaining pressure oscillations in the combustion chamber, or combustion instability, is a commonly encountered and potentially damaging phenomenon in liquid propellant rocket engines (LPREs). In… (more)

Subjects/Keywords: rocket engine; combustion; cryogenic; instabilities; combustion instabilities; liquid rocket

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hardi, J. S. (2012). Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/82071

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):

Hardi, Justin S. “Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.” 2012. Thesis, University of Adelaide. Accessed February 28, 2021. http://hdl.handle.net/2440/82071.

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

MLA Handbook (7th Edition):

Hardi, Justin S. “Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.” 2012. Web. 28 Feb 2021.

Vancouver:

Hardi JS. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. [Internet] [Thesis]. University of Adelaide; 2012. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/2440/82071.

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

Council of Science Editors:

Hardi JS. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. [Thesis]. University of Adelaide; 2012. Available from: http://hdl.handle.net/2440/82071

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


Rochester Institute of Technology

15. Gates, Kevin. CSTARS: Cryogenic CMOS Optical Star Tracking.

Degree: MS, Electrical Engineering, 2020, Rochester Institute of Technology

  CMOS and sCMOS image sensors are a cost-effective alternative to the more common CCD based experimental sensors. While often being less favored than CCDs… (more)

Subjects/Keywords: CMOS; Cryogenic; Rocket attitude; sCMOS; Sounding rocket; Star tracker

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gates, K. (2020). CSTARS: Cryogenic CMOS Optical Star Tracking. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/10611

Chicago Manual of Style (16th Edition):

Gates, Kevin. “CSTARS: Cryogenic CMOS Optical Star Tracking.” 2020. Masters Thesis, Rochester Institute of Technology. Accessed February 28, 2021. https://scholarworks.rit.edu/theses/10611.

MLA Handbook (7th Edition):

Gates, Kevin. “CSTARS: Cryogenic CMOS Optical Star Tracking.” 2020. Web. 28 Feb 2021.

Vancouver:

Gates K. CSTARS: Cryogenic CMOS Optical Star Tracking. [Internet] [Masters thesis]. Rochester Institute of Technology; 2020. [cited 2021 Feb 28]. Available from: https://scholarworks.rit.edu/theses/10611.

Council of Science Editors:

Gates K. CSTARS: Cryogenic CMOS Optical Star Tracking. [Masters Thesis]. Rochester Institute of Technology; 2020. Available from: https://scholarworks.rit.edu/theses/10611


Delft University of Technology

16. Hermsen, R.J.G. (author). Cryogenic propellant tank pressurization.

Degree: 2017, Delft University of Technology

To launch a rocket to the edge of space using a pressure fed rocket system with liquid oxygen as propellant, you need to know exactly… (more)

Subjects/Keywords: cryogenic; high-pressure; propellant; tank pressurization; rocket; Delft Aerospace Rocket Engineering; DARE; pressurant injector; pressure-fed; rocket engine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hermsen, R. J. G. (. (2017). Cryogenic propellant tank pressurization. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:048e34e9-9af6-4b3c-9249-576d192fa7bd

Chicago Manual of Style (16th Edition):

Hermsen, R J G (author). “Cryogenic propellant tank pressurization.” 2017. Masters Thesis, Delft University of Technology. Accessed February 28, 2021. http://resolver.tudelft.nl/uuid:048e34e9-9af6-4b3c-9249-576d192fa7bd.

MLA Handbook (7th Edition):

Hermsen, R J G (author). “Cryogenic propellant tank pressurization.” 2017. Web. 28 Feb 2021.

Vancouver:

Hermsen RJG(. Cryogenic propellant tank pressurization. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Feb 28]. Available from: http://resolver.tudelft.nl/uuid:048e34e9-9af6-4b3c-9249-576d192fa7bd.

Council of Science Editors:

Hermsen RJG(. Cryogenic propellant tank pressurization. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:048e34e9-9af6-4b3c-9249-576d192fa7bd


Brno University of Technology

17. Kadlec, Jan. Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines.

Degree: 2019, Brno University of Technology

 The main aim of this bachelor thesis is developing a search about rocket valves. For better understanding of the function and position valves is chosen… (more)

Subjects/Keywords: raketový ventil; raketový motor; kapalná raketová paliva; hydraulické ztráty; rocket valve; rocket engine; liquid rocket fuels; hydraulic losses

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kadlec, J. (2019). Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/81937

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):

Kadlec, Jan. “Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines.” 2019. Thesis, Brno University of Technology. Accessed February 28, 2021. http://hdl.handle.net/11012/81937.

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

MLA Handbook (7th Edition):

Kadlec, Jan. “Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines.” 2019. Web. 28 Feb 2021.

Vancouver:

Kadlec J. Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/11012/81937.

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

Council of Science Editors:

Kadlec J. Ventily pohonných systémů raketových motorů: Valves of the rocket fuel systems and engines. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/81937

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


Technical University of Lisbon

18. Fidalgo, Andreia Filipa Brito. Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa).

Degree: 2014, Technical University of Lisbon

Mestrado em Engenharia Alimentar - Instituto Superior de Agronomia

In this project the effects of the exposure of rocket (Eruca sativa) to potentially toxic elements… (more)

Subjects/Keywords: rocket; Eruca sativa; cadmium; copper; arsenic; salinity

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Fidalgo, A. F. B. (2014). Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa). (Thesis). Technical University of Lisbon. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/6786

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):

Fidalgo, Andreia Filipa Brito. “Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa).” 2014. Thesis, Technical University of Lisbon. Accessed February 28, 2021. https://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/6786.

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

MLA Handbook (7th Edition):

Fidalgo, Andreia Filipa Brito. “Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa).” 2014. Web. 28 Feb 2021.

Vancouver:

Fidalgo AFB. Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa). [Internet] [Thesis]. Technical University of Lisbon; 2014. [cited 2021 Feb 28]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/6786.

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

Council of Science Editors:

Fidalgo AFB. Exposição e acumulação de elementos potencialmente tóxicos em rúcula (Eruca sativa). [Thesis]. Technical University of Lisbon; 2014. Available from: https://www.rcaap.pt/detail.jsp?id=oai:www.repository.utl.pt:10400.5/6786

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


Anna University

19. Rajesh jesudoss hynes N. Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;.

Degree: Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine, 2015, Anna University

Welding of aluminum based materials to steel is of particular interest to the engineers because the resulting products combine the very different but favourable properties… (more)

Subjects/Keywords: Low cost friction; Rocket fuel tanks

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

N, R. j. h. (2015). Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/50007

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):

N, Rajesh jesudoss hynes. “Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;.” 2015. Thesis, Anna University. Accessed February 28, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/50007.

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

MLA Handbook (7th Edition):

N, Rajesh jesudoss hynes. “Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;.” 2015. Web. 28 Feb 2021.

Vancouver:

N Rjh. Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;. [Internet] [Thesis]. Anna University; 2015. [cited 2021 Feb 28]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/50007.

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

Council of Science Editors:

N Rjh. Investigation on joining of dissimilar materials in a newly developed low cost friction stud welding machine;. [Thesis]. Anna University; 2015. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/50007

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


Penn State University

20. Lin, Chia-Yung. IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS.

Degree: 2010, Penn State University

Rocket nozzle erosion has been a critical issue when rocket motor operating conditions are at high temperature and pressure. During rocket motor operation, nozzle surface… (more)

Subjects/Keywords: rocket nozzle erosion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lin, C. (2010). IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/10841

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):

Lin, Chia-Yung. “IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS.” 2010. Thesis, Penn State University. Accessed February 28, 2021. https://submit-etda.libraries.psu.edu/catalog/10841.

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

MLA Handbook (7th Edition):

Lin, Chia-Yung. “IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS.” 2010. Web. 28 Feb 2021.

Vancouver:

Lin C. IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS. [Internet] [Thesis]. Penn State University; 2010. [cited 2021 Feb 28]. Available from: https://submit-etda.libraries.psu.edu/catalog/10841.

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

Council of Science Editors:

Lin C. IMPORTANT FINDINGS AND OBSERVATIONS OF THE ROCKET NOZZLE EROSION PROCESSES AND THEORETICAL/NUMERICAL SIMULATIONS. [Thesis]. Penn State University; 2010. Available from: https://submit-etda.libraries.psu.edu/catalog/10841

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

21. Cohen, Ian James. The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations.

Degree: PhD, 2015, University of New Hampshire

 Understanding the role that the ionosphere plays in phenomena such as the development of auroral arcs and ion outflow is basic to the investigation of… (more)

Subjects/Keywords: aurora; ionosphere; magnetosphere; rocket; Aeronomy; Geophysics; Physics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cohen, I. J. (2015). The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations. (Doctoral Dissertation). University of New Hampshire. Retrieved from https://scholars.unh.edu/dissertation/2203

Chicago Manual of Style (16th Edition):

Cohen, Ian James. “The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations.” 2015. Doctoral Dissertation, University of New Hampshire. Accessed February 28, 2021. https://scholars.unh.edu/dissertation/2203.

MLA Handbook (7th Edition):

Cohen, Ian James. “The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations.” 2015. Web. 28 Feb 2021.

Vancouver:

Cohen IJ. The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations. [Internet] [Doctoral dissertation]. University of New Hampshire; 2015. [cited 2021 Feb 28]. Available from: https://scholars.unh.edu/dissertation/2203.

Council of Science Editors:

Cohen IJ. The Study of Ionospheric Response to Precipitation Using Sounding Rocket Observations. [Doctoral Dissertation]. University of New Hampshire; 2015. Available from: https://scholars.unh.edu/dissertation/2203


University of KwaZulu-Natal

22. Singh, Nalendran. The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine.

Degree: 2018, University of KwaZulu-Natal

 The deployment of micro- and nanosatellites has greatly increased over the past few decades with advances in miniaturized electronics for communication, imaging and attitude control.… (more)

Subjects/Keywords: Hydrodynamic.; Liquid oxygen.; Impeller.; Rocket engine.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Singh, N. (2018). The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine. (Thesis). University of KwaZulu-Natal. Retrieved from https://researchspace.ukzn.ac.za/handle/10413/17549

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):

Singh, Nalendran. “The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine.” 2018. Thesis, University of KwaZulu-Natal. Accessed February 28, 2021. https://researchspace.ukzn.ac.za/handle/10413/17549.

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

MLA Handbook (7th Edition):

Singh, Nalendran. “The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine.” 2018. Web. 28 Feb 2021.

Vancouver:

Singh N. The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine. [Internet] [Thesis]. University of KwaZulu-Natal; 2018. [cited 2021 Feb 28]. Available from: https://researchspace.ukzn.ac.za/handle/10413/17549.

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

Council of Science Editors:

Singh N. The hydrodynamic design and analysis of a liquid oxygen pump impeller for a rocket engine. [Thesis]. University of KwaZulu-Natal; 2018. Available from: https://researchspace.ukzn.ac.za/handle/10413/17549

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


University of KwaZulu-Natal

23. Theba, Raisa. The development of a paraffin wax/nitrous oxide hybrid rocket slab motor.

Degree: 2019, University of KwaZulu-Natal

 Slab motors are used to determine and investigate the regression rate characteristics of hybrid rocket propellant combinations. This information is fundamental to the overall design… (more)

Subjects/Keywords: Paraffin.; Wax / nitrous.; Hybrid rocket.; Slab motors.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Theba, R. (2019). The development of a paraffin wax/nitrous oxide hybrid rocket slab motor. (Thesis). University of KwaZulu-Natal. Retrieved from https://researchspace.ukzn.ac.za/handle/10413/18105

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):

Theba, Raisa. “The development of a paraffin wax/nitrous oxide hybrid rocket slab motor.” 2019. Thesis, University of KwaZulu-Natal. Accessed February 28, 2021. https://researchspace.ukzn.ac.za/handle/10413/18105.

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

MLA Handbook (7th Edition):

Theba, Raisa. “The development of a paraffin wax/nitrous oxide hybrid rocket slab motor.” 2019. Web. 28 Feb 2021.

Vancouver:

Theba R. The development of a paraffin wax/nitrous oxide hybrid rocket slab motor. [Internet] [Thesis]. University of KwaZulu-Natal; 2019. [cited 2021 Feb 28]. Available from: https://researchspace.ukzn.ac.za/handle/10413/18105.

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

Council of Science Editors:

Theba R. The development of a paraffin wax/nitrous oxide hybrid rocket slab motor. [Thesis]. University of KwaZulu-Natal; 2019. Available from: https://researchspace.ukzn.ac.za/handle/10413/18105

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


University of KwaZulu-Natal

24. Velthuysen, Timothy Johnathan. Closed-loop throttle control of a hybrid rocket motor.

Degree: 2018, University of KwaZulu-Natal

 Hybrid rocket motors produce thrust by reacting a solid fuel with a liquid oxidizer inside a combustion chamber. This approach has certain advantages over conventional… (more)

Subjects/Keywords: Hybrid rocket motors.; Closed-loop testing.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Velthuysen, T. J. (2018). Closed-loop throttle control of a hybrid rocket motor. (Thesis). University of KwaZulu-Natal. Retrieved from https://researchspace.ukzn.ac.za/handle/10413/17862

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):

Velthuysen, Timothy Johnathan. “Closed-loop throttle control of a hybrid rocket motor.” 2018. Thesis, University of KwaZulu-Natal. Accessed February 28, 2021. https://researchspace.ukzn.ac.za/handle/10413/17862.

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

MLA Handbook (7th Edition):

Velthuysen, Timothy Johnathan. “Closed-loop throttle control of a hybrid rocket motor.” 2018. Web. 28 Feb 2021.

Vancouver:

Velthuysen TJ. Closed-loop throttle control of a hybrid rocket motor. [Internet] [Thesis]. University of KwaZulu-Natal; 2018. [cited 2021 Feb 28]. Available from: https://researchspace.ukzn.ac.za/handle/10413/17862.

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

Council of Science Editors:

Velthuysen TJ. Closed-loop throttle control of a hybrid rocket motor. [Thesis]. University of KwaZulu-Natal; 2018. Available from: https://researchspace.ukzn.ac.za/handle/10413/17862

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


Oregon State University

25. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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


University of Surrey

26. Sellers, Jerry Jon. Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites.

Degree: PhD, 1996, University of Surrey

 Affordable small satellites need affordable propulsion systems. The primary objective of this research was to investigate cost-effective propulsion system options for small satellites. The research… (more)

Subjects/Keywords: 621.4356; Rocket motors

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sellers, J. J. (1996). Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites. (Doctoral Dissertation). University of Surrey. Retrieved from http://epubs.surrey.ac.uk/856470/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201

Chicago Manual of Style (16th Edition):

Sellers, Jerry Jon. “Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites.” 1996. Doctoral Dissertation, University of Surrey. Accessed February 28, 2021. http://epubs.surrey.ac.uk/856470/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201.

MLA Handbook (7th Edition):

Sellers, Jerry Jon. “Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites.” 1996. Web. 28 Feb 2021.

Vancouver:

Sellers JJ. Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites. [Internet] [Doctoral dissertation]. University of Surrey; 1996. [cited 2021 Feb 28]. Available from: http://epubs.surrey.ac.uk/856470/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201.

Council of Science Editors:

Sellers JJ. Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites. [Doctoral Dissertation]. University of Surrey; 1996. Available from: http://epubs.surrey.ac.uk/856470/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201

27. Badders, Brian David. Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space.

Degree: MS, Space Studies, 2013, University of North Dakota

  High power rockets and high altitude balloons are two near-space technologies that could be combined in order to provide access to the mesosphere and,… (more)

Subjects/Keywords: balloon; engineering; mesosphere; rocket; rockoon; space

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Badders, B. D. (2013). Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/1502

Chicago Manual of Style (16th Edition):

Badders, Brian David. “Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space.” 2013. Masters Thesis, University of North Dakota. Accessed February 28, 2021. https://commons.und.edu/theses/1502.

MLA Handbook (7th Edition):

Badders, Brian David. “Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space.” 2013. Web. 28 Feb 2021.

Vancouver:

Badders BD. Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space. [Internet] [Masters thesis]. University of North Dakota; 2013. [cited 2021 Feb 28]. Available from: https://commons.und.edu/theses/1502.

Council of Science Editors:

Badders BD. Developing Hybrid Near-Space Technologies For Affordable Access To Suborbital Space. [Masters Thesis]. University of North Dakota; 2013. Available from: https://commons.und.edu/theses/1502


University of Bristol

28. Cobbald, T. J. The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates.

Degree: PhD, 1985, University of Bristol

Subjects/Keywords: 621.4356; Rocket motors

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cobbald, T. J. (1985). The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates. (Doctoral Dissertation). University of Bristol. Retrieved from http://hdl.handle.net/1983/d67c1e71-1605-4bcc-b268-0cdf3ed9f470

Chicago Manual of Style (16th Edition):

Cobbald, T J. “The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates.” 1985. Doctoral Dissertation, University of Bristol. Accessed February 28, 2021. http://hdl.handle.net/1983/d67c1e71-1605-4bcc-b268-0cdf3ed9f470.

MLA Handbook (7th Edition):

Cobbald, T J. “The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates.” 1985. Web. 28 Feb 2021.

Vancouver:

Cobbald TJ. The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates. [Internet] [Doctoral dissertation]. University of Bristol; 1985. [cited 2021 Feb 28]. Available from: http://hdl.handle.net/1983/d67c1e71-1605-4bcc-b268-0cdf3ed9f470.

Council of Science Editors:

Cobbald TJ. The impingement of underexpanded, axisymmetric, rocket motor exhausts and cold jets on flat plates. [Doctoral Dissertation]. University of Bristol; 1985. Available from: http://hdl.handle.net/1983/d67c1e71-1605-4bcc-b268-0cdf3ed9f470


Cranfield University

29. Dennis, C. W. A study of rocket exhaust particles.

Degree: PhD, 1996, Cranfield University

 The exhaust plumes generated by rocket motors are of significant military importance for missile detection, recognition and communication due to their electromagnetic emission and propagation… (more)

Subjects/Keywords: 621.4356; Rocket motors

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Dennis, C. W. (1996). A study of rocket exhaust particles. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/3583 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336464

Chicago Manual of Style (16th Edition):

Dennis, C W. “A study of rocket exhaust particles.” 1996. Doctoral Dissertation, Cranfield University. Accessed February 28, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/3583 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336464.

MLA Handbook (7th Edition):

Dennis, C W. “A study of rocket exhaust particles.” 1996. Web. 28 Feb 2021.

Vancouver:

Dennis CW. A study of rocket exhaust particles. [Internet] [Doctoral dissertation]. Cranfield University; 1996. [cited 2021 Feb 28]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3583 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336464.

Council of Science Editors:

Dennis CW. A study of rocket exhaust particles. [Doctoral Dissertation]. Cranfield University; 1996. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3583 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336464


Delft University of Technology

30. Motsyk, O.O. (author). Design of a Solid Rocket Motor for a Transonic Research Vehicle.

Degree: 2015, Delft University of Technology

Hypresearch is a project that has been under development with the collaboration of ATG Europe, TU Delft, TNO for the past 7+ years. The eventual… (more)

Subjects/Keywords: SRM; rocket; motor; propulsion; design; MAIT

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Motsyk, O. O. (. (2015). Design of a Solid Rocket Motor for a Transonic Research Vehicle. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b5480136-5082-44fb-9a42-f29e5a3027c5

Chicago Manual of Style (16th Edition):

Motsyk, O O (author). “Design of a Solid Rocket Motor for a Transonic Research Vehicle.” 2015. Masters Thesis, Delft University of Technology. Accessed February 28, 2021. http://resolver.tudelft.nl/uuid:b5480136-5082-44fb-9a42-f29e5a3027c5.

MLA Handbook (7th Edition):

Motsyk, O O (author). “Design of a Solid Rocket Motor for a Transonic Research Vehicle.” 2015. Web. 28 Feb 2021.

Vancouver:

Motsyk OO(. Design of a Solid Rocket Motor for a Transonic Research Vehicle. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Feb 28]. Available from: http://resolver.tudelft.nl/uuid:b5480136-5082-44fb-9a42-f29e5a3027c5.

Council of Science Editors:

Motsyk OO(. Design of a Solid Rocket Motor for a Transonic Research Vehicle. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:b5480136-5082-44fb-9a42-f29e5a3027c5

[1] [2] [3] [4] [5] … [14]

.