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You searched for subject:(Propellants). Showing records 1 – 30 of 77 total matches.

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University of Kashmir

1. 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

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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 November 25, 2020. 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. 25 Nov 2020.

Vancouver:

Arora AJ. Combustion studies on solid Rocket Propellants Phenol Formaldehyde composite Systems;. [Internet] [Thesis]. University of Kashmir; 2014. [cited 2020 Nov 25]. 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


Penn State University

2. Saksena, Pulkit. Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors.

Degree: 2014, Penn State University

 The testing of hypergolic propellants has been carried out for decades and the use of hypergolic propellants at a systems level is very well understood.… (more)

Subjects/Keywords: Hypergolic; Propellants; Combustion; Microfluidic; Microreactor

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APA (6th Edition):

Saksena, P. (2014). Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/22410

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):

Saksena, Pulkit. “Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors.” 2014. Thesis, Penn State University. Accessed November 25, 2020. https://submit-etda.libraries.psu.edu/catalog/22410.

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

MLA Handbook (7th Edition):

Saksena, Pulkit. “Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors.” 2014. Web. 25 Nov 2020.

Vancouver:

Saksena P. Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors. [Internet] [Thesis]. Penn State University; 2014. [cited 2020 Nov 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/22410.

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

Council of Science Editors:

Saksena P. Study of Condensed Phase Reactions Between Hypergolic Propellants using Microreactors. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/22410

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


University of Arizona

3. Turner, Stewart William, 1936-. The effect of electrostatic fields on flame spread rates of solid propellant .

Degree: 1970, University of Arizona

Subjects/Keywords: Solid propellants.

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APA (6th Edition):

Turner, Stewart William, 1. (1970). The effect of electrostatic fields on flame spread rates of solid propellant . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/565210

Chicago Manual of Style (16th Edition):

Turner, Stewart William, 1936-. “The effect of electrostatic fields on flame spread rates of solid propellant .” 1970. Doctoral Dissertation, University of Arizona. Accessed November 25, 2020. http://hdl.handle.net/10150/565210.

MLA Handbook (7th Edition):

Turner, Stewart William, 1936-. “The effect of electrostatic fields on flame spread rates of solid propellant .” 1970. Web. 25 Nov 2020.

Vancouver:

Turner, Stewart William 1. The effect of electrostatic fields on flame spread rates of solid propellant . [Internet] [Doctoral dissertation]. University of Arizona; 1970. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10150/565210.

Council of Science Editors:

Turner, Stewart William 1. The effect of electrostatic fields on flame spread rates of solid propellant . [Doctoral Dissertation]. University of Arizona; 1970. Available from: http://hdl.handle.net/10150/565210


University of Arizona

4. Gosch, Damian Leigh. Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils .

Degree: 2012, University of Arizona

 During military operations, a small fraction of propellant mass is not consumed during firing and is deposited onto the ground surface. Soluble propellant constituents can… (more)

Subjects/Keywords: fate; propellants; sorption; transport; Hydrology; batch; contaminants

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APA (6th Edition):

Gosch, D. L. (2012). Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/228473

Chicago Manual of Style (16th Edition):

Gosch, Damian Leigh. “Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils .” 2012. Masters Thesis, University of Arizona. Accessed November 25, 2020. http://hdl.handle.net/10150/228473.

MLA Handbook (7th Edition):

Gosch, Damian Leigh. “Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils .” 2012. Web. 25 Nov 2020.

Vancouver:

Gosch DL. Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils . [Internet] [Masters thesis]. University of Arizona; 2012. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10150/228473.

Council of Science Editors:

Gosch DL. Determining Fate and Transport Parameters for Nitroglycerine, 2,4-Dinitrotoluene, 2,6-Dinitrotoluene and Nitroguanidine in Soils . [Masters Thesis]. University of Arizona; 2012. Available from: http://hdl.handle.net/10150/228473


Georgia Tech

5. Sessa, Paul Anthony. Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds.

Degree: PhD, Chemical Engineering, 1970, Georgia Tech

Subjects/Keywords: Mass spectrometry; Propellants

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APA (6th Edition):

Sessa, P. A. (1970). Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10243

Chicago Manual of Style (16th Edition):

Sessa, Paul Anthony. “Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds.” 1970. Doctoral Dissertation, Georgia Tech. Accessed November 25, 2020. http://hdl.handle.net/1853/10243.

MLA Handbook (7th Edition):

Sessa, Paul Anthony. “Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds.” 1970. Web. 25 Nov 2020.

Vancouver:

Sessa PA. Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds. [Internet] [Doctoral dissertation]. Georgia Tech; 1970. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1853/10243.

Council of Science Editors:

Sessa PA. Mass spectrometric investigation of the synthesis and molecular energetics of nitrogen-oxygen-fluorine compounds. [Doctoral Dissertation]. Georgia Tech; 1970. Available from: http://hdl.handle.net/1853/10243


Georgia Tech

6. Varney, Al Michael. An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants.

Degree: PhD, Aerospace Engineering, 1970, Georgia Tech

Subjects/Keywords: Combustion; Solid propellants

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APA (6th Edition):

Varney, A. M. (1970). An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12530

Chicago Manual of Style (16th Edition):

Varney, Al Michael. “An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants.” 1970. Doctoral Dissertation, Georgia Tech. Accessed November 25, 2020. http://hdl.handle.net/1853/12530.

MLA Handbook (7th Edition):

Varney, Al Michael. “An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants.” 1970. Web. 25 Nov 2020.

Vancouver:

Varney AM. An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants. [Internet] [Doctoral dissertation]. Georgia Tech; 1970. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1853/12530.

Council of Science Editors:

Varney AM. An experimental investigation of the burning mechanisms of ammonium perchlorate composite solid propellants. [Doctoral Dissertation]. Georgia Tech; 1970. Available from: http://hdl.handle.net/1853/12530

7. Indiana, Clément. Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants.

Degree: Docteur es, Energétique, thermique, combustion, 2016, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique

Les processus physiques qui régissent la pulvérisation de sprays constituent la première étape vers une compréhension globale du comportement de moteurs fusées à ergols stockables.… (more)

Subjects/Keywords: Ergols stockables; Injecteurs à impact; Staorable propellants; Impinging-jet injectors

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APA (6th Edition):

Indiana, C. (2016). Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants. (Doctoral Dissertation). Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Retrieved from http://www.theses.fr/2016ESMA0025

Chicago Manual of Style (16th Edition):

Indiana, Clément. “Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants.” 2016. Doctoral Dissertation, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Accessed November 25, 2020. http://www.theses.fr/2016ESMA0025.

MLA Handbook (7th Edition):

Indiana, Clément. “Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants.” 2016. Web. 25 Nov 2020.

Vancouver:

Indiana C. Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants. [Internet] [Doctoral dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2016. [cited 2020 Nov 25]. Available from: http://www.theses.fr/2016ESMA0025.

Council of Science Editors:

Indiana C. Caractérisation expérimentale de la pulvérisation, de l'allumage et de la combustion de bi-ergols. Application à la propulsion spatiale par ergols stockables : Experimental Characterisation of the Spraying, the Ignition and, the Combustion of Bi-Propellants. Application to Space Propulsion With Storable Propellants. [Doctoral Dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2016. Available from: http://www.theses.fr/2016ESMA0025


University of Utah

8. Perez, Jesus Paulo L. Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications.

Degree: PhD, Chemistry, 2013, University of Utah

 Boron’s energy potential as a combustion fuel can be harnessed by using nanosize solidparticulates. In this study, functionalized boron nanoparticles were produced through highyieldball milling… (more)

Subjects/Keywords: Boron nanoparticles; Fuel additive; Ionic liquids; Propellants; X-ray photoelectron spectroscopy

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APA (6th Edition):

Perez, J. P. L. (2013). Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications. (Doctoral Dissertation). University of Utah. Retrieved from http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/3489/rec/1945

Chicago Manual of Style (16th Edition):

Perez, Jesus Paulo L. “Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications.” 2013. Doctoral Dissertation, University of Utah. Accessed November 25, 2020. http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/3489/rec/1945.

MLA Handbook (7th Edition):

Perez, Jesus Paulo L. “Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications.” 2013. Web. 25 Nov 2020.

Vancouver:

Perez JPL. Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications. [Internet] [Doctoral dissertation]. University of Utah; 2013. [cited 2020 Nov 25]. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/3489/rec/1945.

Council of Science Editors:

Perez JPL. Preparation and characterization of surface functionalized boron nanoparticles for fuel and propellant applications. [Doctoral Dissertation]. University of Utah; 2013. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/3489/rec/1945


Texas A&M University

9. Homan-Cruz, Gabriel Dylan. Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives.

Degree: MS, Mechanical Engineering, 2015, Texas A&M University

 Aqueous solutions of hydroxylammonium nitrate (HAN) are promising as possible replacements for hydrazine as liquid rocket propellants. HAN-based propellants offer lower toxicity, higher density, and… (more)

Subjects/Keywords: hydroxylammonium nitrate; HAN; liquid monopropellants; rocket propellants; combustion; burning rates; nanoparticles

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APA (6th Edition):

Homan-Cruz, G. D. (2015). Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156185

Chicago Manual of Style (16th Edition):

Homan-Cruz, Gabriel Dylan. “Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives.” 2015. Masters Thesis, Texas A&M University. Accessed November 25, 2020. http://hdl.handle.net/1969.1/156185.

MLA Handbook (7th Edition):

Homan-Cruz, Gabriel Dylan. “Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives.” 2015. Web. 25 Nov 2020.

Vancouver:

Homan-Cruz GD. Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives. [Internet] [Masters thesis]. Texas A&M University; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1969.1/156185.

Council of Science Editors:

Homan-Cruz GD. Experimental Techniques to Study the Combustion of Aqueous Solutions of Hydroxylammonium Nitrate with Additives. [Masters Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/156185


Penn State University

10. Weismiller, Michael Raymond. Characterization of Ammonia Borane for Chemical Propulsion Applications.

Degree: 2012, Penn State University

 Ammonia borane (NH3BH3; AB), which has a hydrogen content of 19.6% by weight, has been studied recently as a potential means of hydrogen storage for… (more)

Subjects/Keywords: Energetic materials; Novel propellants; Hydrogen storage; Hybrid rocket; Boron

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APA (6th Edition):

Weismiller, M. R. (2012). Characterization of Ammonia Borane for Chemical Propulsion Applications. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15486

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):

Weismiller, Michael Raymond. “Characterization of Ammonia Borane for Chemical Propulsion Applications.” 2012. Thesis, Penn State University. Accessed November 25, 2020. https://submit-etda.libraries.psu.edu/catalog/15486.

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

MLA Handbook (7th Edition):

Weismiller, Michael Raymond. “Characterization of Ammonia Borane for Chemical Propulsion Applications.” 2012. Web. 25 Nov 2020.

Vancouver:

Weismiller MR. Characterization of Ammonia Borane for Chemical Propulsion Applications. [Internet] [Thesis]. Penn State University; 2012. [cited 2020 Nov 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/15486.

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

Council of Science Editors:

Weismiller MR. Characterization of Ammonia Borane for Chemical Propulsion Applications. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/15486

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


Cranfield University

11. 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 November 25, 2020. 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. 25 Nov 2020.

Vancouver:

Tucker J. A whole life assessment of extruded double base propellants. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2020 Nov 25]. 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

12. 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 November 25, 2020. 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. 25 Nov 2020.

Vancouver:

Tucker J. A whole life assessment of extruded double base propellants. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2020 Nov 25]. 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

13. Shen, Jeffrey D. Examination of the small scale slow cookoff behavior of a cast modified double base propellant.

Degree: MS, Mechanical Engineering, 2015, University of Illinois – Urbana-Champaign

 The slow cookoff behavior of a proprietary cast modified double base (CMDB) propellant was examined using a variety of diagnostic techniques with the ultimate goal… (more)

Subjects/Keywords: Cookoff; Solid Propellants

…Homogenous propellants are typically categorized as single or double base depending on… …their composition. Single base propellants are generally composed nitrate esters such as… …Double base (DB) propellants combine NC and nitroglycerin (NG, C3H5N3O9)… …for added energy. Triple base propellants frequently appear in artillery applications with… …propellants. Many homogenous propellants also contain stabilizers, curing agents, and burn rate… 

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APA (6th Edition):

Shen, J. D. (2015). Examination of the small scale slow cookoff behavior of a cast modified double base propellant. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/78439

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):

Shen, Jeffrey D. “Examination of the small scale slow cookoff behavior of a cast modified double base propellant.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed November 25, 2020. http://hdl.handle.net/2142/78439.

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

MLA Handbook (7th Edition):

Shen, Jeffrey D. “Examination of the small scale slow cookoff behavior of a cast modified double base propellant.” 2015. Web. 25 Nov 2020.

Vancouver:

Shen JD. Examination of the small scale slow cookoff behavior of a cast modified double base propellant. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/2142/78439.

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

Council of Science Editors:

Shen JD. Examination of the small scale slow cookoff behavior of a cast modified double base propellant. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/78439

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


University of Arizona

14. Daly, Robert Francis, 1928-. Current theories of solid propellant combustion instability .

Degree: 1962, University of Arizona

Subjects/Keywords: Combustion  – Research.; Solid propellants.

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APA (6th Edition):

Daly, Robert Francis, 1. (1962). Current theories of solid propellant combustion instability . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/319396

Chicago Manual of Style (16th Edition):

Daly, Robert Francis, 1928-. “Current theories of solid propellant combustion instability .” 1962. Masters Thesis, University of Arizona. Accessed November 25, 2020. http://hdl.handle.net/10150/319396.

MLA Handbook (7th Edition):

Daly, Robert Francis, 1928-. “Current theories of solid propellant combustion instability .” 1962. Web. 25 Nov 2020.

Vancouver:

Daly, Robert Francis 1. Current theories of solid propellant combustion instability . [Internet] [Masters thesis]. University of Arizona; 1962. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10150/319396.

Council of Science Editors:

Daly, Robert Francis 1. Current theories of solid propellant combustion instability . [Masters Thesis]. University of Arizona; 1962. Available from: http://hdl.handle.net/10150/319396


University of Arizona

15. Towson, Earl Raymond, 1938-. The effects of acceleration upon the linear burning rate of solid-rocket propellants .

Degree: 1965, University of Arizona

Subjects/Keywords: Rockets (Aeronautics)  – Fuel.; Solid propellants.

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APA (6th Edition):

Towson, Earl Raymond, 1. (1965). The effects of acceleration upon the linear burning rate of solid-rocket propellants . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/347514

Chicago Manual of Style (16th Edition):

Towson, Earl Raymond, 1938-. “The effects of acceleration upon the linear burning rate of solid-rocket propellants .” 1965. Masters Thesis, University of Arizona. Accessed November 25, 2020. http://hdl.handle.net/10150/347514.

MLA Handbook (7th Edition):

Towson, Earl Raymond, 1938-. “The effects of acceleration upon the linear burning rate of solid-rocket propellants .” 1965. Web. 25 Nov 2020.

Vancouver:

Towson, Earl Raymond 1. The effects of acceleration upon the linear burning rate of solid-rocket propellants . [Internet] [Masters thesis]. University of Arizona; 1965. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10150/347514.

Council of Science Editors:

Towson, Earl Raymond 1. The effects of acceleration upon the linear burning rate of solid-rocket propellants . [Masters Thesis]. University of Arizona; 1965. Available from: http://hdl.handle.net/10150/347514


California State University – Northridge

16. Cheng, Ming-hua. Ram-rocket propulsion system with subsonic combustion.

Degree: MS, Department of Engineering, 1984, California State University – Northridge

 This project analyzes the performance of the ram-rocket with subsonic combustion in terms of propellant-air ratio, flight Mach number and altitude. The theoretical analysis of… (more)

Subjects/Keywords: Propellants; Dissertations, Academic  – CSUN  – Engineering

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APA (6th Edition):

Cheng, M. (1984). Ram-rocket propulsion system with subsonic combustion. (Masters Thesis). California State University – Northridge. Retrieved from http://hdl.handle.net/10211.3/128844

Chicago Manual of Style (16th Edition):

Cheng, Ming-hua. “Ram-rocket propulsion system with subsonic combustion.” 1984. Masters Thesis, California State University – Northridge. Accessed November 25, 2020. http://hdl.handle.net/10211.3/128844.

MLA Handbook (7th Edition):

Cheng, Ming-hua. “Ram-rocket propulsion system with subsonic combustion.” 1984. Web. 25 Nov 2020.

Vancouver:

Cheng M. Ram-rocket propulsion system with subsonic combustion. [Internet] [Masters thesis]. California State University – Northridge; 1984. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10211.3/128844.

Council of Science Editors:

Cheng M. Ram-rocket propulsion system with subsonic combustion. [Masters Thesis]. California State University – Northridge; 1984. Available from: http://hdl.handle.net/10211.3/128844


Georgia Tech

17. Handley, J. C. (John Charles). An experimental investigation of catalysis in the combustion of composite solid propellants.

Degree: PhD, Aeronautical Engineering, 1976, Georgia Tech

Subjects/Keywords: Solid propellants; Copper catalysts

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APA (6th Edition):

Handley, J. C. (. C. (1976). An experimental investigation of catalysis in the combustion of composite solid propellants. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12911

Chicago Manual of Style (16th Edition):

Handley, J C (John Charles). “An experimental investigation of catalysis in the combustion of composite solid propellants.” 1976. Doctoral Dissertation, Georgia Tech. Accessed November 25, 2020. http://hdl.handle.net/1853/12911.

MLA Handbook (7th Edition):

Handley, J C (John Charles). “An experimental investigation of catalysis in the combustion of composite solid propellants.” 1976. Web. 25 Nov 2020.

Vancouver:

Handley JC(C. An experimental investigation of catalysis in the combustion of composite solid propellants. [Internet] [Doctoral dissertation]. Georgia Tech; 1976. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1853/12911.

Council of Science Editors:

Handley JC(C. An experimental investigation of catalysis in the combustion of composite solid propellants. [Doctoral Dissertation]. Georgia Tech; 1976. Available from: http://hdl.handle.net/1853/12911


Georgia Tech

18. Jones, Howard Evans. An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants.

Degree: PhD, Aerospace Engineering, 1971, Georgia Tech

Subjects/Keywords: Solid propellants; Combustion Research

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APA (6th Edition):

Jones, H. E. (1971). An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12950

Chicago Manual of Style (16th Edition):

Jones, Howard Evans. “An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants.” 1971. Doctoral Dissertation, Georgia Tech. Accessed November 25, 2020. http://hdl.handle.net/1853/12950.

MLA Handbook (7th Edition):

Jones, Howard Evans. “An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants.” 1971. Web. 25 Nov 2020.

Vancouver:

Jones HE. An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants. [Internet] [Doctoral dissertation]. Georgia Tech; 1971. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1853/12950.

Council of Science Editors:

Jones HE. An experimental investigation relating to the combustion mechanism of ammonium perchlorate propellants. [Doctoral Dissertation]. Georgia Tech; 1971. Available from: http://hdl.handle.net/1853/12950


Indian Institute of Science

19. Reshmi, S. Investigations on Azide Functional Polymers as Binders for Solid Propellants.

Degree: PhD, Faculty of Science, 2018, Indian Institute of Science

 This thesis contains investigations in the area of polymers herein propellants binders are modified functionally to meet the requirements of future energetic propellants. Chapter 1… (more)

Subjects/Keywords: Solid Propellants; Propellants Binders; Azide Functional Polymers; Click Chemistry; Diazides; Solid Propellant Binders; Polymeric Binders; Diazido Ester; Glycidyl Azide Polymer; Solid Propellant Binder; Inorganic Chemistry

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APA (6th Edition):

Reshmi, S. (2018). Investigations on Azide Functional Polymers as Binders for Solid Propellants. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3506

Chicago Manual of Style (16th Edition):

Reshmi, S. “Investigations on Azide Functional Polymers as Binders for Solid Propellants.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed November 25, 2020. http://etd.iisc.ac.in/handle/2005/3506.

MLA Handbook (7th Edition):

Reshmi, S. “Investigations on Azide Functional Polymers as Binders for Solid Propellants.” 2018. Web. 25 Nov 2020.

Vancouver:

Reshmi S. Investigations on Azide Functional Polymers as Binders for Solid Propellants. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2020 Nov 25]. Available from: http://etd.iisc.ac.in/handle/2005/3506.

Council of Science Editors:

Reshmi S. Investigations on Azide Functional Polymers as Binders for Solid Propellants. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3506


Indian Institute of Science

20. Oommen, Charlie. Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions.

Degree: PhD, Faculty of Engineering, 2012, Indian Institute of Science

Subjects/Keywords: Solid Propellants; Rockets (Aeronautics) - Fuel; Ammonium Nitrate; Propellants; Diepoxide; Epoxy Resins; Oxidizers; Aeronautics

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APA (6th Edition):

Oommen, C. (2012). Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1769

Chicago Manual of Style (16th Edition):

Oommen, Charlie. “Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions.” 2012. Doctoral Dissertation, Indian Institute of Science. Accessed November 25, 2020. http://etd.iisc.ac.in/handle/2005/1769.

MLA Handbook (7th Edition):

Oommen, Charlie. “Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions.” 2012. Web. 25 Nov 2020.

Vancouver:

Oommen C. Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2012. [cited 2020 Nov 25]. Available from: http://etd.iisc.ac.in/handle/2005/1769.

Council of Science Editors:

Oommen C. Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions. [Doctoral Dissertation]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ac.in/handle/2005/1769


Universidade Estadual de Campinas

21. Libardi, Juliano. Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene.

Degree: 2009, Universidade Estadual de Campinas

 Abstract: The hydroxyl-terminated (HTPB) based solid composite propellant used in the production of solid rocket motors, developed in the Institute of Aeronautics and Space (IAE),… (more)

Subjects/Keywords: Propelentes; Difusão; Plastificante; Propellants; Diffusion; Plastificizer

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APA (6th Edition):

Libardi, J. (2009). Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene. (Thesis). Universidade Estadual de Campinas. Retrieved from http://repositorio.unicamp.br/jspui/handle/REPOSIP/267117

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):

Libardi, Juliano. “Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene.” 2009. Thesis, Universidade Estadual de Campinas. Accessed November 25, 2020. http://repositorio.unicamp.br/jspui/handle/REPOSIP/267117.

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

MLA Handbook (7th Edition):

Libardi, Juliano. “Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene.” 2009. Web. 25 Nov 2020.

Vancouver:

Libardi J. Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene. [Internet] [Thesis]. Universidade Estadual de Campinas; 2009. [cited 2020 Nov 25]. Available from: http://repositorio.unicamp.br/jspui/handle/REPOSIP/267117.

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

Council of Science Editors:

Libardi J. Estudos do fenomeno de difusão de plastificantes em propelente composito a base de polibutadiero hidroxilado utilizado em motores foguete: A study of diffusion of plasticizer in a solid propellant based on hydroxyl-terminated polybutadiene. [Thesis]. Universidade Estadual de Campinas; 2009. Available from: http://repositorio.unicamp.br/jspui/handle/REPOSIP/267117

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


University of Washington

22. Mejia Montano, Diego. Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster.

Degree: 2019, University of Washington

 Pulsed Plasma Thrusters typically live in the low-range efficiency realm compared to other types of electric propulsion thrusters. In an attempt to explore if any… (more)

Subjects/Keywords: novel propellants; physics; plasma; propulsion; thruster; Plasma physics; Aerospace engineering; Applied mathematics; Aeronautics and astronautics

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APA (6th Edition):

Mejia Montano, D. (2019). Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/44006

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):

Mejia Montano, Diego. “Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster.” 2019. Thesis, University of Washington. Accessed November 25, 2020. http://hdl.handle.net/1773/44006.

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

MLA Handbook (7th Edition):

Mejia Montano, Diego. “Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster.” 2019. Web. 25 Nov 2020.

Vancouver:

Mejia Montano D. Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster. [Internet] [Thesis]. University of Washington; 2019. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1773/44006.

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

Council of Science Editors:

Mejia Montano D. Characterization of An Exploding Micro-Wire Pulsed Plasma Thruster. [Thesis]. University of Washington; 2019. Available from: http://hdl.handle.net/1773/44006

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

23. Le Brize, Axel. Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants.

Degree: Docteur es, Sciences des matériaux, 2017, Université de Strasbourg

Les travaux de thèse présentés dans ce manuscrit ont porté sur l’élaboration et la caractérisation de poudres propulsives à sensibilités réduites. Ceci a été effectué… (more)

Subjects/Keywords: Spray évaporation flash; Poudres propulsives; Nanomatériaux; Désensibilisation; Spray evaporation flash; Propellants; Nanomaterials; Desensitization; 662.1; 531.3

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APA (6th Edition):

Le Brize, A. (2017). Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants. (Doctoral Dissertation). Université de Strasbourg. Retrieved from http://www.theses.fr/2017STRAE020

Chicago Manual of Style (16th Edition):

Le Brize, Axel. “Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants.” 2017. Doctoral Dissertation, Université de Strasbourg. Accessed November 25, 2020. http://www.theses.fr/2017STRAE020.

MLA Handbook (7th Edition):

Le Brize, Axel. “Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants.” 2017. Web. 25 Nov 2020.

Vancouver:

Le Brize A. Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants. [Internet] [Doctoral dissertation]. Université de Strasbourg; 2017. [cited 2020 Nov 25]. Available from: http://www.theses.fr/2017STRAE020.

Council of Science Editors:

Le Brize A. Etude de la nanostructuration de matériaux énergétiques multi-composants pour application aux poudres propulsives à sensibilités réduites : Study of the nanostructuration of multi-component energetic materials for application to low vulnerability propellants. [Doctoral Dissertation]. Université de Strasbourg; 2017. Available from: http://www.theses.fr/2017STRAE020


University of Arizona

24. Perez, Daniel Lizarraga. Scientific predictability of solid rocket performance: Analyses of the processing parameters.

Degree: 1992, University of Arizona

 The objective of this dissertation is to present a computational model of the suspensions composing uncured composite solid propellant. The work examined highly concentrated suspensions… (more)

Subjects/Keywords: Dissertations, Academic.; Aerospace engineering.; Solid propellants.

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APA (6th Edition):

Perez, D. L. (1992). Scientific predictability of solid rocket performance: Analyses of the processing parameters. (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/185817

Chicago Manual of Style (16th Edition):

Perez, Daniel Lizarraga. “Scientific predictability of solid rocket performance: Analyses of the processing parameters. ” 1992. Doctoral Dissertation, University of Arizona. Accessed November 25, 2020. http://hdl.handle.net/10150/185817.

MLA Handbook (7th Edition):

Perez, Daniel Lizarraga. “Scientific predictability of solid rocket performance: Analyses of the processing parameters. ” 1992. Web. 25 Nov 2020.

Vancouver:

Perez DL. Scientific predictability of solid rocket performance: Analyses of the processing parameters. [Internet] [Doctoral dissertation]. University of Arizona; 1992. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10150/185817.

Council of Science Editors:

Perez DL. Scientific predictability of solid rocket performance: Analyses of the processing parameters. [Doctoral Dissertation]. University of Arizona; 1992. Available from: http://hdl.handle.net/10150/185817


Virginia Tech

25. Tanaka, Martin Lyn. Influence of storage environment upon crack opening and growth in composite solid rocket propellant.

Degree: MS, Engineering Mechanics, 1993, Virginia Tech

Subjects/Keywords: Solid propellants; LD5655.V855 1993.T362

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APA (6th Edition):

Tanaka, M. L. (1993). Influence of storage environment upon crack opening and growth in composite solid rocket propellant. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/40723

Chicago Manual of Style (16th Edition):

Tanaka, Martin Lyn. “Influence of storage environment upon crack opening and growth in composite solid rocket propellant.” 1993. Masters Thesis, Virginia Tech. Accessed November 25, 2020. http://hdl.handle.net/10919/40723.

MLA Handbook (7th Edition):

Tanaka, Martin Lyn. “Influence of storage environment upon crack opening and growth in composite solid rocket propellant.” 1993. Web. 25 Nov 2020.

Vancouver:

Tanaka ML. Influence of storage environment upon crack opening and growth in composite solid rocket propellant. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10919/40723.

Council of Science Editors:

Tanaka ML. Influence of storage environment upon crack opening and growth in composite solid rocket propellant. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/40723


Virginia Tech

26. Mouille, Hervé. Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant.

Degree: MS, Engineering Science and Mechanics, 1992, Virginia Tech

need OCR Advisors/Committee Members: Smith, Charles W. (committeechair).

Subjects/Keywords: Solid propellants; LD5655.V855 1992.M684

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APA (6th Edition):

Mouille, H. (1992). Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43774

Chicago Manual of Style (16th Edition):

Mouille, Hervé. “Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant.” 1992. Masters Thesis, Virginia Tech. Accessed November 25, 2020. http://hdl.handle.net/10919/43774.

MLA Handbook (7th Edition):

Mouille, Hervé. “Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant.” 1992. Web. 25 Nov 2020.

Vancouver:

Mouille H. Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant. [Internet] [Masters thesis]. Virginia Tech; 1992. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10919/43774.

Council of Science Editors:

Mouille H. Influence of strain rate and temperature upon the mechanical and fracture behavior of a simulated solid propellant. [Masters Thesis]. Virginia Tech; 1992. Available from: http://hdl.handle.net/10919/43774


Virginia Tech

27. Wang, Lei. Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation.

Degree: PhD, Engineering Mechanics, 1992, Virginia Tech

Subjects/Keywords: Solid propellants.; LD5655.V856 1992.W362

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APA (6th Edition):

Wang, L. (1992). Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/38641

Chicago Manual of Style (16th Edition):

Wang, Lei. “Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation.” 1992. Doctoral Dissertation, Virginia Tech. Accessed November 25, 2020. http://hdl.handle.net/10919/38641.

MLA Handbook (7th Edition):

Wang, Lei. “Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation.” 1992. Web. 25 Nov 2020.

Vancouver:

Wang L. Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation. [Internet] [Doctoral dissertation]. Virginia Tech; 1992. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/10919/38641.

Council of Science Editors:

Wang L. Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation. [Doctoral Dissertation]. Virginia Tech; 1992. Available from: http://hdl.handle.net/10919/38641


Texas A&M University

28. Fuller, Andrew Lee. A study of the critical temperatures of smokeless propellants.

Degree: MS, industrial safety, 2012, Texas A&M University

Subjects/Keywords: industrial safety.; Major industrial safety.; Propellants.; Gunpowder, Smokeless.

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APA (6th Edition):

Fuller, A. L. (2012). A study of the critical temperatures of smokeless propellants. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1980-THESIS-F965

Chicago Manual of Style (16th Edition):

Fuller, Andrew Lee. “A study of the critical temperatures of smokeless propellants.” 2012. Masters Thesis, Texas A&M University. Accessed November 25, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1980-THESIS-F965.

MLA Handbook (7th Edition):

Fuller, Andrew Lee. “A study of the critical temperatures of smokeless propellants.” 2012. Web. 25 Nov 2020.

Vancouver:

Fuller AL. A study of the critical temperatures of smokeless propellants. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Nov 25]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1980-THESIS-F965.

Council of Science Editors:

Fuller AL. A study of the critical temperatures of smokeless propellants. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1980-THESIS-F965

29. Gabriel, Vladimir Hallak. Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima.

Degree: Mestrado, Processos Catalíticos e Biocatalíticos, 2014, University of São Paulo

Propelentes sólidos são materiais energéticos que produzem gases em alta pressão por meio de uma reação de combustão. Qualquer propelente sólido inclui dois ou mais… (more)

Subjects/Keywords: ballistic modifiers; burning rate; Double-Base propellants; Modificadores balísticos; Propelentes Base Dupla - BD; velocidade de queima

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APA (6th Edition):

Gabriel, V. H. (2014). Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/97/97137/tde-30042014-094502/ ;

Chicago Manual of Style (16th Edition):

Gabriel, Vladimir Hallak. “Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima.” 2014. Masters Thesis, University of São Paulo. Accessed November 25, 2020. http://www.teses.usp.br/teses/disponiveis/97/97137/tde-30042014-094502/ ;.

MLA Handbook (7th Edition):

Gabriel, Vladimir Hallak. “Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima.” 2014. Web. 25 Nov 2020.

Vancouver:

Gabriel VH. Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima. [Internet] [Masters thesis]. University of São Paulo; 2014. [cited 2020 Nov 25]. Available from: http://www.teses.usp.br/teses/disponiveis/97/97137/tde-30042014-094502/ ;.

Council of Science Editors:

Gabriel VH. Estudo de modificadores balísticos na formulação de propelentes base dupla visando à otimização de sua velocidade de queima. [Masters Thesis]. University of São Paulo; 2014. Available from: http://www.teses.usp.br/teses/disponiveis/97/97137/tde-30042014-094502/ ;


Penn State University

30. Kudva, Gautam Narendra. A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure.

Degree: 2008, Penn State University

 This work was part of a larger program aimed at understanding and modeling propellant combustion and its interaction with changes in pressure and velocity in… (more)

Subjects/Keywords: laser-driven; response measurements; solid propellants; pressure-driven

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APA (6th Edition):

Kudva, G. N. (2008). A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/5839

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):

Kudva, Gautam Narendra. “A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure.” 2008. Thesis, Penn State University. Accessed November 25, 2020. https://submit-etda.libraries.psu.edu/catalog/5839.

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

MLA Handbook (7th Edition):

Kudva, Gautam Narendra. “A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure.” 2008. Web. 25 Nov 2020.

Vancouver:

Kudva GN. A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure. [Internet] [Thesis]. Penn State University; 2008. [cited 2020 Nov 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/5839.

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

Council of Science Editors:

Kudva GN. A Study of Laser and Pressure-Driven Response Measurements for Solid Propellants at Low Pressure. [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/5839

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

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