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You searched for subject:(Thermal Protection System). Showing records 1 – 30 of 40 total matches.

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Delft University of Technology

1. Roorda, Evelyne (author). Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer.

Degree: 2017, Delft University of Technology

 During its lifetime a space launcher is subjected to extreme heat loads. To protect space vehicles from these heat loads and their resulting temperatures they… (more)

Subjects/Keywords: spaceplane; thermal protection system; SSTO

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APA (6th Edition):

Roorda, E. (. (2017). Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dbd513c7-346d-4a7b-972c-7eb9497f1bd8

Chicago Manual of Style (16th Edition):

Roorda, Evelyne (author). “Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer.” 2017. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:dbd513c7-346d-4a7b-972c-7eb9497f1bd8.

MLA Handbook (7th Edition):

Roorda, Evelyne (author). “Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer.” 2017. Web. 01 Mar 2021.

Vancouver:

Roorda E(. Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:dbd513c7-346d-4a7b-972c-7eb9497f1bd8.

Council of Science Editors:

Roorda E(. Thermal Protection System Analysis and Sizing for Spaceplane Configurations: Preliminary design of the TPS and optimization of the insulation layer. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:dbd513c7-346d-4a7b-972c-7eb9497f1bd8


University of Manchester

2. Cong, Yuhang. Synchronized measurement technology supported operational tripping schemes.

Degree: PhD, 2016, University of Manchester

 The increasing volume of renewable and intermittent generation that is being connected to power systems means that system operators need more advanced dynamic control tools… (more)

Subjects/Keywords: 621.319; Conductor/Transformer Heating; Dynamic Thermal Line Rating; Operational Tripping Scheme; Power System Protection; Power System; System Integrity Protection Scheme

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APA (6th Edition):

Cong, Y. (2016). Synchronized measurement technology supported operational tripping schemes. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/synchronized-measurement-technology-supported-operational-tripping-schemes(7d472659-d352-4291-96fc-fce7e6ce5fc8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.722280

Chicago Manual of Style (16th Edition):

Cong, Yuhang. “Synchronized measurement technology supported operational tripping schemes.” 2016. Doctoral Dissertation, University of Manchester. Accessed March 01, 2021. https://www.research.manchester.ac.uk/portal/en/theses/synchronized-measurement-technology-supported-operational-tripping-schemes(7d472659-d352-4291-96fc-fce7e6ce5fc8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.722280.

MLA Handbook (7th Edition):

Cong, Yuhang. “Synchronized measurement technology supported operational tripping schemes.” 2016. Web. 01 Mar 2021.

Vancouver:

Cong Y. Synchronized measurement technology supported operational tripping schemes. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Mar 01]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/synchronized-measurement-technology-supported-operational-tripping-schemes(7d472659-d352-4291-96fc-fce7e6ce5fc8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.722280.

Council of Science Editors:

Cong Y. Synchronized measurement technology supported operational tripping schemes. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/synchronized-measurement-technology-supported-operational-tripping-schemes(7d472659-d352-4291-96fc-fce7e6ce5fc8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.722280


University of Waterloo

3. Christopher, Nicholas. Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate.

Degree: 2020, University of Waterloo

 Transpiration cooling is a promising thermal protection system for gas turbines, atmospheric re-entry heat shields, and rocket engine combustion chambers. Design of transpiration cooling systems… (more)

Subjects/Keywords: rocket; thermal protection system; transpiration cooling; direct numerical simulation

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APA (6th Edition):

Christopher, N. (2020). Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/15463

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):

Christopher, Nicholas. “Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate.” 2020. Thesis, University of Waterloo. Accessed March 01, 2021. http://hdl.handle.net/10012/15463.

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

MLA Handbook (7th Edition):

Christopher, Nicholas. “Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate.” 2020. Web. 01 Mar 2021.

Vancouver:

Christopher N. Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate. [Internet] [Thesis]. University of Waterloo; 2020. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10012/15463.

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

Council of Science Editors:

Christopher N. Numerical Analysis of Transpiration Cooling on a Turbulent Flat Plate. [Thesis]. University of Waterloo; 2020. Available from: http://hdl.handle.net/10012/15463

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


University of Vermont

4. Smith, Silas. Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility.

Degree: MS, Mechanical Engineering, 2013, University of Vermont

 Inductively Coupled Plasma (ICP) facilities create high enthalpy ows to recreate atmospheric entry conditions. Although no condition has been duplicated exactly in a ground test… (more)

Subjects/Keywords: subsonic; heat flux; inductively coupled plasma; supersonic; thermal protection system

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APA (6th Edition):

Smith, S. (2013). Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility. (Thesis). University of Vermont. Retrieved from https://scholarworks.uvm.edu/graddis/218

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):

Smith, Silas. “Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility.” 2013. Thesis, University of Vermont. Accessed March 01, 2021. https://scholarworks.uvm.edu/graddis/218.

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

MLA Handbook (7th Edition):

Smith, Silas. “Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility.” 2013. Web. 01 Mar 2021.

Vancouver:

Smith S. Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility. [Internet] [Thesis]. University of Vermont; 2013. [cited 2021 Mar 01]. Available from: https://scholarworks.uvm.edu/graddis/218.

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

Council of Science Editors:

Smith S. Investigation of Subsonic and Supersonic Flow Characteristics of an Inductively Coupled Plasma Facility. [Thesis]. University of Vermont; 2013. Available from: https://scholarworks.uvm.edu/graddis/218

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


Delft University of Technology

5. Ahuja, Aditi (author). Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design.

Degree: 2020, Delft University of Technology

The next step in spaceflight, among others, is the development of a reusable launch vehicle (RLV) suitable for manned missions. All existing designs of re-entry… (more)

Subjects/Keywords: Active thermal protection system; Reusable launch vehicle; Conceptual design

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APA (6th Edition):

Ahuja, A. (. (2020). Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a61aff50-928c-458b-856d-41d075f853b1

Chicago Manual of Style (16th Edition):

Ahuja, Aditi (author). “Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design.” 2020. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:a61aff50-928c-458b-856d-41d075f853b1.

MLA Handbook (7th Edition):

Ahuja, Aditi (author). “Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design.” 2020. Web. 01 Mar 2021.

Vancouver:

Ahuja A(. Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:a61aff50-928c-458b-856d-41d075f853b1.

Council of Science Editors:

Ahuja A(. Active Thermal Protection System for Reusable Launch Vehicle: A Conceptual Design. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:a61aff50-928c-458b-856d-41d075f853b1


Texas A&M University

6. Gesting, Peter Paul. A photogrammetric on-orbit inspection for orbiter thermal protection system.

Degree: MS, Aerospace Engineering, 2006, Texas A&M University

 Due to the Columbia Space Shuttle Accident of February 2003, the Columbia Accident Investigation Board determined the need for an on-orbit inspection system for the… (more)

Subjects/Keywords: Image Processing; Photogrammetry; Thermal Protection System

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APA (6th Edition):

Gesting, P. P. (2006). A photogrammetric on-orbit inspection for orbiter thermal protection system. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/3191

Chicago Manual of Style (16th Edition):

Gesting, Peter Paul. “A photogrammetric on-orbit inspection for orbiter thermal protection system.” 2006. Masters Thesis, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/3191.

MLA Handbook (7th Edition):

Gesting, Peter Paul. “A photogrammetric on-orbit inspection for orbiter thermal protection system.” 2006. Web. 01 Mar 2021.

Vancouver:

Gesting PP. A photogrammetric on-orbit inspection for orbiter thermal protection system. [Internet] [Masters thesis]. Texas A&M University; 2006. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/3191.

Council of Science Editors:

Gesting PP. A photogrammetric on-orbit inspection for orbiter thermal protection system. [Masters Thesis]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/3191


Delft University of Technology

7. Dubois, Wouter (author). Enhanced Radiation Cooling: Design of an active thermal protection system.

Degree: 2017, Delft University of Technology

 Current-day space vehicle are equipped with a passive Thermal Protection System (TPS), but these systems operate at the edge of their capabilities. The research into… (more)

Subjects/Keywords: Active thermal protection system; Enhanced radiation cooling; 6 Degree of Freedom modelling

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APA (6th Edition):

Dubois, W. (. (2017). Enhanced Radiation Cooling: Design of an active thermal protection system. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979

Chicago Manual of Style (16th Edition):

Dubois, Wouter (author). “Enhanced Radiation Cooling: Design of an active thermal protection system.” 2017. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979.

MLA Handbook (7th Edition):

Dubois, Wouter (author). “Enhanced Radiation Cooling: Design of an active thermal protection system.” 2017. Web. 01 Mar 2021.

Vancouver:

Dubois W(. Enhanced Radiation Cooling: Design of an active thermal protection system. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979.

Council of Science Editors:

Dubois W(. Enhanced Radiation Cooling: Design of an active thermal protection system. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979


University of Illinois – Urbana-Champaign

8. Harpale, Abhilash. Scale-bridging molecular dynamics simulations of plasma-surface interactions.

Degree: PhD, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign

 Plasma processing of materials plays a vital part in electronic, aerospace, automobile, metal manufacturing and biomedical industries. Plasma-surface interactions can be divided into two categories:… (more)

Subjects/Keywords: graphene; plasma; molecular dynamics; atomic scale simulations; surfaces; thermal protection system; NASA; spacecraft

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APA (6th Edition):

Harpale, A. (2018). Scale-bridging molecular dynamics simulations of plasma-surface interactions. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/100909

Chicago Manual of Style (16th Edition):

Harpale, Abhilash. “Scale-bridging molecular dynamics simulations of plasma-surface interactions.” 2018. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed March 01, 2021. http://hdl.handle.net/2142/100909.

MLA Handbook (7th Edition):

Harpale, Abhilash. “Scale-bridging molecular dynamics simulations of plasma-surface interactions.” 2018. Web. 01 Mar 2021.

Vancouver:

Harpale A. Scale-bridging molecular dynamics simulations of plasma-surface interactions. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2018. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2142/100909.

Council of Science Editors:

Harpale A. Scale-bridging molecular dynamics simulations of plasma-surface interactions. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/100909


University of Maryland

9. Beerman, Adam Farrell. THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN.

Degree: Aerospace Engineering, 2011, University of Maryland

 Gas-surface modeling is dependent on material type and atmospheric reentry conditions. Lower molecular collisions at the low pressure trajectories make it more likely for occurrences… (more)

Subjects/Keywords: Aerospace Engineering; ablation; aerothermodynamics; finite-rate reaction; hypersonics; recession; thermal protection system

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APA (6th Edition):

Beerman, A. F. (2011). THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/11515

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):

Beerman, Adam Farrell. “THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN.” 2011. Thesis, University of Maryland. Accessed March 01, 2021. http://hdl.handle.net/1903/11515.

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

MLA Handbook (7th Edition):

Beerman, Adam Farrell. “THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN.” 2011. Web. 01 Mar 2021.

Vancouver:

Beerman AF. THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN. [Internet] [Thesis]. University of Maryland; 2011. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1903/11515.

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

Council of Science Editors:

Beerman AF. THE EFFECTS OF FINITE-RATE REACTIONS AT THE GAS/SURFACE INTERFACE IN SUPPORT OF THERMAL PROTECTION SYSTEM DESIGN. [Thesis]. University of Maryland; 2011. Available from: http://hdl.handle.net/1903/11515

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


Penn State University

10. Weir, Erik David. DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT.

Degree: 2010, Penn State University

 A prototype wireless sensor system is developed to collect data from sensors that are of importance on space platforms, and also important in the testing… (more)

Subjects/Keywords: wireless sensor system; zigbee; thermal protection system; thermocouple

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APA (6th Edition):

Weir, E. D. (2010). DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11235

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):

Weir, Erik David. “DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT.” 2010. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/11235.

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

MLA Handbook (7th Edition):

Weir, Erik David. “DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT.” 2010. Web. 01 Mar 2021.

Vancouver:

Weir ED. DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT. [Internet] [Thesis]. Penn State University; 2010. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/11235.

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

Council of Science Editors:

Weir ED. DESIGN AND APPLICATIONS OF ZIGBEE-ENABLED WIRELESS SENSOR SYSTEMS FOR A SPACE RELEVANT ENVIRONMENT. [Thesis]. Penn State University; 2010. Available from: https://submit-etda.libraries.psu.edu/catalog/11235

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


University of Vermont

11. Owens, Walten. Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch.

Degree: PhD, Mechanical Engineering, 2015, University of Vermont

  Flexible thermal protection systems are of interest due to their necessity for the success of future atmospheric entry vehicles. Current non-ablative flexible designs incorporate… (more)

Subjects/Keywords: Catalycity; Oxidation; SiC; Silicon Carbide; Thermal Protection System; TPS; Aerospace Engineering; Mechanical Engineering; Mechanics of Materials

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APA (6th Edition):

Owens, W. (2015). Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch. (Doctoral Dissertation). University of Vermont. Retrieved from https://scholarworks.uvm.edu/graddis/363

Chicago Manual of Style (16th Edition):

Owens, Walten. “Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch.” 2015. Doctoral Dissertation, University of Vermont. Accessed March 01, 2021. https://scholarworks.uvm.edu/graddis/363.

MLA Handbook (7th Edition):

Owens, Walten. “Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch.” 2015. Web. 01 Mar 2021.

Vancouver:

Owens W. Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch. [Internet] [Doctoral dissertation]. University of Vermont; 2015. [cited 2021 Mar 01]. Available from: https://scholarworks.uvm.edu/graddis/363.

Council of Science Editors:

Owens W. Aero-Thermal Characterization Of Silicon Carbide Flexible Tps Using A 30kw Icp Torch. [Doctoral Dissertation]. University of Vermont; 2015. Available from: https://scholarworks.uvm.edu/graddis/363


Delft University of Technology

12. Buursink, J. On the development of a cooled metallic thermal protection system for spacecraft.

Degree: 2005, Delft University of Technology

 To achieve a significant cost reduction for launch of payloads to space, it is essential that the launcher is reused to the largest possible extent,… (more)

Subjects/Keywords: thermal protection system; water cooling; reusable launcher

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APA (6th Edition):

Buursink, J. (2005). On the development of a cooled metallic thermal protection system for spacecraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf

Chicago Manual of Style (16th Edition):

Buursink, J. “On the development of a cooled metallic thermal protection system for spacecraft.” 2005. Doctoral Dissertation, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf.

MLA Handbook (7th Edition):

Buursink, J. “On the development of a cooled metallic thermal protection system for spacecraft.” 2005. Web. 01 Mar 2021.

Vancouver:

Buursink J. On the development of a cooled metallic thermal protection system for spacecraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2005. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf.

Council of Science Editors:

Buursink J. On the development of a cooled metallic thermal protection system for spacecraft. [Doctoral Dissertation]. Delft University of Technology; 2005. Available from: http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; urn:NBN:nl:ui:24-uuid:8f648295-c060-4575-80ab-a2cd175813cf ; http://resolver.tudelft.nl/uuid:8f648295-c060-4575-80ab-a2cd175813cf


University of Michigan

13. Ng, Wei Heok. Thermomechanical Analysis of a Damaged Thermal Protection System.

Degree: PhD, Aerospace Engineering, 2007, University of Michigan

 Research on the effects of damage on the thermomechanical performance and structural integrity of thermal protection systems (TPS) has been limited. The objective of this… (more)

Subjects/Keywords: Thermal Protection System; Finite Element; Thermal Stress; Heat Transfer; Aerospace Engineering; Engineering

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APA (6th Edition):

Ng, W. H. (2007). Thermomechanical Analysis of a Damaged Thermal Protection System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/57597

Chicago Manual of Style (16th Edition):

Ng, Wei Heok. “Thermomechanical Analysis of a Damaged Thermal Protection System.” 2007. Doctoral Dissertation, University of Michigan. Accessed March 01, 2021. http://hdl.handle.net/2027.42/57597.

MLA Handbook (7th Edition):

Ng, Wei Heok. “Thermomechanical Analysis of a Damaged Thermal Protection System.” 2007. Web. 01 Mar 2021.

Vancouver:

Ng WH. Thermomechanical Analysis of a Damaged Thermal Protection System. [Internet] [Doctoral dissertation]. University of Michigan; 2007. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2027.42/57597.

Council of Science Editors:

Ng WH. Thermomechanical Analysis of a Damaged Thermal Protection System. [Doctoral Dissertation]. University of Michigan; 2007. Available from: http://hdl.handle.net/2027.42/57597

14. Le Foll, Sébastien. Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature.

Degree: Docteur es, Thermique et énergétique, 2014, INSA Lyon

Les travaux présentés dans cette thèse CIFRE financée par AIRBUS Defence & Space s’intègrent dans une problématique de développement de nouveaux Systèmes de Protection Thermique… (more)

Subjects/Keywords: Thermique; Rentrée atmosphérique; Haute température; Système de protection thermique; Propriété radiative; Pyrolyse; Conductivité thermique; Rayonnement thermique; Carbone; Silice; Thermics; Atmospheric entry; High temperature; Thermal protection system; Radiative properties; Pyrolysis; Thermal conductivity; Heat transfer; Carbon; Silica; 536.230 72

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APA (6th Edition):

Le Foll, S. (2014). Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature. (Doctoral Dissertation). INSA Lyon. Retrieved from http://www.theses.fr/2014ISAL0079

Chicago Manual of Style (16th Edition):

Le Foll, Sébastien. “Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature.” 2014. Doctoral Dissertation, INSA Lyon. Accessed March 01, 2021. http://www.theses.fr/2014ISAL0079.

MLA Handbook (7th Edition):

Le Foll, Sébastien. “Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature.” 2014. Web. 01 Mar 2021.

Vancouver:

Le Foll S. Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature. [Internet] [Doctoral dissertation]. INSA Lyon; 2014. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2014ISAL0079.

Council of Science Editors:

Le Foll S. Modélisation du couplage conduction/rayonnement dans les systèmes de protection thermique soumis à de très hauts niveaux de températures : Coupled radiative/conductive heat transfer modeling in thermal protection systems at high temperature. [Doctoral Dissertation]. INSA Lyon; 2014. Available from: http://www.theses.fr/2014ISAL0079

15. -9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and friction heat the surrounding air to temperatures in excess of 6,000… (more)

Subjects/Keywords: Raman scattering; Plasma; ICP; Pyrolysis; Inductively coupled plasma; Ablation; Thermal protection system; Thermal protection; Charring ablator

…Spectroscopy .................................................... 22 1.3 Thermal Protection System… …thermal protection system mass in the overall spacecraft launch mass was the Galileo Probe… …give is that the instrumentation on the Galileo probe thermal protection system indicated… …developed for thermal protection system testing in the Soviet Union, with two facilities, IPG-1… …that the most important factor in the design of a thermal protection system is heat transfer… 

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APA (6th Edition):

-9034-9438. (2018). Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/72664

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-9034-9438. “Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 01, 2021. http://hdl.handle.net/2152/72664.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-9034-9438. “Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.” 2018. Web. 01 Mar 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2152/72664.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/72664

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Indian Institute of Science

16. Ajith, M R. Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications.

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

 A porous silica –silica composite was processed with varying fiber diameters using the slurry moulding technique. The advantage of the process was that the density… (more)

Subjects/Keywords: Silica-Silica Porous Composites; Calcium Strontium Zirconium Phosphaste Ceramics; Ceramics, Thermal Protection System; Amorphous Silica Fibers; Silica Fibers; Silica Composites; Silica Matrix Composites; CSZP; Ca0.5Sr0.5Zr4P6O24; Silica-Sllica Composites; Materials Science

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APA (6th Edition):

Ajith, M. R. (2018). Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3901

Chicago Manual of Style (16th Edition):

Ajith, M R. “Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/3901.

MLA Handbook (7th Edition):

Ajith, M R. “Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications.” 2018. Web. 01 Mar 2021.

Vancouver:

Ajith MR. Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/3901.

Council of Science Editors:

Ajith MR. Synthesis and Characterization of Silica-Silica Porous Composite and Calcium Strontium Zirconium Phosphate Ceramics for Thermal Protection Applications. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3901


University of Vermont

17. Dougherty, Maximilian. Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch.

Degree: PhD, Mechanical Engineering, 2015, University of Vermont

  In the design of a thermal protection system for atmospheric entry, aerothermal heating presents a major impediment to efficient heat shield design. Recombination of… (more)

Subjects/Keywords: chemical nonequilibrium; finite rate chemistry; inductively coupled plasma; planetary entry; surface catalycity; thermal protection system; Aerospace Engineering; Mechanical Engineering; Plasma and Beam Physics

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APA (6th Edition):

Dougherty, M. (2015). Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch. (Doctoral Dissertation). University of Vermont. Retrieved from https://scholarworks.uvm.edu/graddis/512

Chicago Manual of Style (16th Edition):

Dougherty, Maximilian. “Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch.” 2015. Doctoral Dissertation, University of Vermont. Accessed March 01, 2021. https://scholarworks.uvm.edu/graddis/512.

MLA Handbook (7th Edition):

Dougherty, Maximilian. “Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch.” 2015. Web. 01 Mar 2021.

Vancouver:

Dougherty M. Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch. [Internet] [Doctoral dissertation]. University of Vermont; 2015. [cited 2021 Mar 01]. Available from: https://scholarworks.uvm.edu/graddis/512.

Council of Science Editors:

Dougherty M. Numerical Simulations of Reacting Flow in an Inductively Coupled Plasma Torch. [Doctoral Dissertation]. University of Vermont; 2015. Available from: https://scholarworks.uvm.edu/graddis/512


University of Central Florida

18. Snapp, Cooper. Evaluation Of Space Shuttle Tile Subnominal Bonds.

Degree: 2006, University of Central Florida

 This study researched the history of Space Shuttle Reusable Surface Insulation which was designed and developed for use on the United States Orbiter fleet to… (more)

Subjects/Keywords: Space Shuttle; Thermal Protection System; tile; Orbiter; subnominal bond; Aerospace Engineering; Engineering

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APA (6th Edition):

Snapp, C. (2006). Evaluation Of Space Shuttle Tile Subnominal Bonds. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/831

Chicago Manual of Style (16th Edition):

Snapp, Cooper. “Evaluation Of Space Shuttle Tile Subnominal Bonds.” 2006. Masters Thesis, University of Central Florida. Accessed March 01, 2021. https://stars.library.ucf.edu/etd/831.

MLA Handbook (7th Edition):

Snapp, Cooper. “Evaluation Of Space Shuttle Tile Subnominal Bonds.” 2006. Web. 01 Mar 2021.

Vancouver:

Snapp C. Evaluation Of Space Shuttle Tile Subnominal Bonds. [Internet] [Masters thesis]. University of Central Florida; 2006. [cited 2021 Mar 01]. Available from: https://stars.library.ucf.edu/etd/831.

Council of Science Editors:

Snapp C. Evaluation Of Space Shuttle Tile Subnominal Bonds. [Masters Thesis]. University of Central Florida; 2006. Available from: https://stars.library.ucf.edu/etd/831


University of Kentucky

19. Smith, David L. Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials.

Degree: 2016, University of Kentucky

 The Mars Science Laboratory Entry Descent and Landing Instrumentation (MEDLI) project performed extensive arc jet tests for development, qualification, and calibration of instrumented heat shield… (more)

Subjects/Keywords: atmospheric entry; thermal protection system; material response; numerical heat transfer; arc jet testing; experimental modeling; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Heat Transfer, Combustion; Other Mechanical Engineering; Space Vehicles

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APA (6th Edition):

Smith, D. L. (2016). Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/83

Chicago Manual of Style (16th Edition):

Smith, David L. “Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials.” 2016. Masters Thesis, University of Kentucky. Accessed March 01, 2021. https://uknowledge.uky.edu/me_etds/83.

MLA Handbook (7th Edition):

Smith, David L. “Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials.” 2016. Web. 01 Mar 2021.

Vancouver:

Smith DL. Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials. [Internet] [Masters thesis]. University of Kentucky; 2016. [cited 2021 Mar 01]. Available from: https://uknowledge.uky.edu/me_etds/83.

Council of Science Editors:

Smith DL. Comparisons of Ablator Experimental Performance to Response Modeling and Effects of Water Phase Transition in Porous TPS Materials. [Masters Thesis]. University of Kentucky; 2016. Available from: https://uknowledge.uky.edu/me_etds/83


University of Kentucky

20. Sparks, James Devin. The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights.

Degree: 2018, University of Kentucky

 The Kentucky Re-entry Universal Payload System (KRUPS) is an adaptable testbed for atmosphere entry science experiments, with an initial application to thermal protection systems (TPS).… (more)

Subjects/Keywords: Thermal Protection System (TPS); Sounding Rocket; International Space Station (ISS); Re-entry Vehicle; Aviation and Space Education; Computer-Aided Engineering and Design; Heat Transfer, Combustion; Manufacturing

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APA (6th Edition):

Sparks, J. D. (2018). The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/123

Chicago Manual of Style (16th Edition):

Sparks, James Devin. “The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights.” 2018. Masters Thesis, University of Kentucky. Accessed March 01, 2021. https://uknowledge.uky.edu/me_etds/123.

MLA Handbook (7th Edition):

Sparks, James Devin. “The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights.” 2018. Web. 01 Mar 2021.

Vancouver:

Sparks JD. The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights. [Internet] [Masters thesis]. University of Kentucky; 2018. [cited 2021 Mar 01]. Available from: https://uknowledge.uky.edu/me_etds/123.

Council of Science Editors:

Sparks JD. The Kentucky Re-entry Universal Payload System (KRUPS): Sub-orbital Flights. [Masters Thesis]. University of Kentucky; 2018. Available from: https://uknowledge.uky.edu/me_etds/123


University of Kentucky

21. Davuluri, Raghava Sai Chaitanya. Modeling of spallation phenomenon in an arc-jet environment.

Degree: 2015, University of Kentucky

 Space vehicles, while entering the planetary atmosphere, experience high loads of heat. Ablative materials are commonly used for a thermal protection system, which undergo mass… (more)

Subjects/Keywords: atmospheric entry; thermal protection system; ablation; spallation; Aerodynamics and Fluid Mechanics; Computational Engineering; Heat Transfer, Combustion; Numerical Analysis and Scientific Computing; Thermodynamics

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APA (6th Edition):

Davuluri, R. S. C. (2015). Modeling of spallation phenomenon in an arc-jet environment. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/63

Chicago Manual of Style (16th Edition):

Davuluri, Raghava Sai Chaitanya. “Modeling of spallation phenomenon in an arc-jet environment.” 2015. Masters Thesis, University of Kentucky. Accessed March 01, 2021. https://uknowledge.uky.edu/me_etds/63.

MLA Handbook (7th Edition):

Davuluri, Raghava Sai Chaitanya. “Modeling of spallation phenomenon in an arc-jet environment.” 2015. Web. 01 Mar 2021.

Vancouver:

Davuluri RSC. Modeling of spallation phenomenon in an arc-jet environment. [Internet] [Masters thesis]. University of Kentucky; 2015. [cited 2021 Mar 01]. Available from: https://uknowledge.uky.edu/me_etds/63.

Council of Science Editors:

Davuluri RSC. Modeling of spallation phenomenon in an arc-jet environment. [Masters Thesis]. University of Kentucky; 2015. Available from: https://uknowledge.uky.edu/me_etds/63


University of Cincinnati

22. Sockalingam, Subramani. Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA.

Degree: MS, Engineering : Mechanical Engineering, 2008, University of Cincinnati

 A frame work has been setup for the simulation of hypersonic reentry vehicles using commercial codes FLUENT and LS-DYNA. The main goal of this work… (more)

Subjects/Keywords: Mechanical Engineering; Hypersonic Reentry Vehicles; Thermal Protection System TPS; Ablation

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APA (6th Edition):

Sockalingam, S. (2008). Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218801526

Chicago Manual of Style (16th Edition):

Sockalingam, Subramani. “Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA.” 2008. Masters Thesis, University of Cincinnati. Accessed March 01, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218801526.

MLA Handbook (7th Edition):

Sockalingam, Subramani. “Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA.” 2008. Web. 01 Mar 2021.

Vancouver:

Sockalingam S. Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA. [Internet] [Masters thesis]. University of Cincinnati; 2008. [cited 2021 Mar 01]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218801526.

Council of Science Editors:

Sockalingam S. Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA. [Masters Thesis]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218801526


University of Kentucky

23. Nichols, James Tyler. The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight.

Degree: 2021, University of Kentucky

 Due to the uniqueness of atmospheric entry environments, ground facilities cannot accurately replicate re-entry conditions. Consequently, scientists primarily rely on numerical models to predict these… (more)

Subjects/Keywords: Thermal Protection System; TPS; Cygnus; International Space Station; ISS; Re-entry Vehicle; Atmospheric Entry; Space Vehicles; Structures and Materials; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Nichols, J. T. (2021). The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/165

Chicago Manual of Style (16th Edition):

Nichols, James Tyler. “The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight.” 2021. Masters Thesis, University of Kentucky. Accessed March 01, 2021. https://uknowledge.uky.edu/me_etds/165.

MLA Handbook (7th Edition):

Nichols, James Tyler. “The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight.” 2021. Web. 01 Mar 2021.

Vancouver:

Nichols JT. The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight. [Internet] [Masters thesis]. University of Kentucky; 2021. [cited 2021 Mar 01]. Available from: https://uknowledge.uky.edu/me_etds/165.

Council of Science Editors:

Nichols JT. The Kentucky Re-Entry Universal Payload System (KRUPS): Orbital Flight. [Masters Thesis]. University of Kentucky; 2021. Available from: https://uknowledge.uky.edu/me_etds/165

24. Marley, Christopher. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 Due to the large aerodynamic heating at high Mach numbers, Thermal Protection System (TPS) design considerations are critical for hypersonic vehicles, and engineers seek to… (more)

Subjects/Keywords: Hypersonic Cruise Vehicle; Active Thermal Protection System (TPS); Passive Thermal Protection System (TPS); Scramjet; Aerospace Engineering; Engineering

…the thermal protection system, compared to the present work… …10 3.1 Passive thermal protection system layers for results shown in Figs. 3.3, 3.4… …external surface passive thermal protection system for cruise at M∞ = 8, q∞ = 60 kPa… …69 Maximum temperatures in vehicle external surface passive thermal protection system at M… …x5D; energy [J] specific enthalpy [J/kg], thermal protection system… 

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APA (6th Edition):

Marley, C. (2018). Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/144038

Chicago Manual of Style (16th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Doctoral Dissertation, University of Michigan. Accessed March 01, 2021. http://hdl.handle.net/2027.42/144038.

MLA Handbook (7th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Web. 01 Mar 2021.

Vancouver:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2027.42/144038.

Council of Science Editors:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/144038

25. Cong, Yuhang. Synchronized Measurement Technology Supported Operational Tripping Schemes.

Degree: 2016, University of Manchester

 The increasing volume of renewable and intermittent generation that is being connected to power systems means that system operators need more advanced dynamic control tools… (more)

Subjects/Keywords: Power System; Power System Protection; System Integrity Protection Scheme; Operational Tripping Scheme; Dynamic Thermal Line Rating; Conductor/Transformer Heating

…considered to be intelligent, adaptive and efficient SIPS for the thermal protection of system… …thermal protection scheme. If a disturbance occurs in the power system, the post-fault current… …conventional thermal protection schemes and understand the thermal behaviour of system elements… …thermal protection of system elements. As such, they can be considered as a typical Smart Grid… …this thesis is to design intelligent system integrity protection schemes (SIPS)… 

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APA (6th Edition):

Cong, Y. (2016). Synchronized Measurement Technology Supported Operational Tripping Schemes. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:301116

Chicago Manual of Style (16th Edition):

Cong, Yuhang. “Synchronized Measurement Technology Supported Operational Tripping Schemes.” 2016. Doctoral Dissertation, University of Manchester. Accessed March 01, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:301116.

MLA Handbook (7th Edition):

Cong, Yuhang. “Synchronized Measurement Technology Supported Operational Tripping Schemes.” 2016. Web. 01 Mar 2021.

Vancouver:

Cong Y. Synchronized Measurement Technology Supported Operational Tripping Schemes. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Mar 01]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:301116.

Council of Science Editors:

Cong Y. Synchronized Measurement Technology Supported Operational Tripping Schemes. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:301116


Université de Bordeaux I

26. Nguyen, Huy Cuong. Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers.

Degree: Docteur es, Automatique et productique, signal et image, 2013, Université de Bordeaux I

Sur les différents calculateurs du véhicule, de plus en plus d'organes sont commandés par un interrupteur en silicium (circuit MOSFET) au lieu d'un relais. En… (more)

Subjects/Keywords: Mosfet; Câblage; Modélisation électrothermique; Protection; Court-circuits; Dérivation non-entière; Estimateurs; Dimensionnement de système électrique; Electronique automobile; Contrôle/commande; Electrothermique; Fusibles; Mosfet; Harness; Thermal electrical modeling; Protection; Short circuit; Estimation; Fractional derivative; Sizing electric; Car electronic system; Control; Smart fuse; Mosfet

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APA (6th Edition):

Nguyen, H. C. (2013). Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers. (Doctoral Dissertation). Université de Bordeaux I. Retrieved from http://www.theses.fr/2013BOR14776

Chicago Manual of Style (16th Edition):

Nguyen, Huy Cuong. “Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers.” 2013. Doctoral Dissertation, Université de Bordeaux I. Accessed March 01, 2021. http://www.theses.fr/2013BOR14776.

MLA Handbook (7th Edition):

Nguyen, Huy Cuong. “Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers.” 2013. Web. 01 Mar 2021.

Vancouver:

Nguyen HC. Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers. [Internet] [Doctoral dissertation]. Université de Bordeaux I; 2013. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2013BOR14776.

Council of Science Editors:

Nguyen HC. Modélisation électrothermique de système électrique électronique automobile et pilotage de mosfet intelligents pour protéger les faisceaux, éviter les courts circuits aggravés et diminuer la masse de câblage : The experience of the visit and construction of knowledge : the case of science museums and scientific cultural centers. [Doctoral Dissertation]. Université de Bordeaux I; 2013. Available from: http://www.theses.fr/2013BOR14776


Brno University of Technology

27. Konečná, Petra. Domov pro seniory v Telnici: Pension for the Elderly in Telnice.

Degree: 2019, Brno University of Technology

 Topic of this master’s thesis is a retirement house in village Telnice. The project was designed directly for village Telnice according to their requirements. It… (more)

Subjects/Keywords: Domov pro seniory; Sedlová střecha; Plochá střecha; Zděný systém; Kontaktní zateplovací systém; Tepelná technika; Požární ochrana budovy; Betonové konstrukce; Kanalizace; Retirement house; Saddle roof; Flat roof; Brick masonry; Thermal insulation system; Thermal protection of building; Fire safety of building; Concrete constructions; Sewerage

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

APA (6th Edition):

Konečná, P. (2019). Domov pro seniory v Telnici: Pension for the Elderly in Telnice. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/29735

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):

Konečná, Petra. “Domov pro seniory v Telnici: Pension for the Elderly in Telnice.” 2019. Thesis, Brno University of Technology. Accessed March 01, 2021. http://hdl.handle.net/11012/29735.

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

MLA Handbook (7th Edition):

Konečná, Petra. “Domov pro seniory v Telnici: Pension for the Elderly in Telnice.” 2019. Web. 01 Mar 2021.

Vancouver:

Konečná P. Domov pro seniory v Telnici: Pension for the Elderly in Telnice. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/11012/29735.

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

Council of Science Editors:

Konečná P. Domov pro seniory v Telnici: Pension for the Elderly in Telnice. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/29735

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

28. Zinner, Evan J. Assessment of aerocapture-entry trajectories for human Mars exploration.

Degree: MS, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

 Using aerocapture to insert into an elliptic parking orbit prior to entry, descent, and landing is being explored for human Mars missions. These aerocapture-entry trajectories… (more)

Subjects/Keywords: Mars Entry Descent Landing Human Exploration Aerocapture Aerocapture-entry TPS Thermal Protection System Parking Orbit

…Mars. [7] Figure. 3: Illustration of ablative thermal protection system [10… …component of the lift vector. 11 The thermal protection system (TPS) material on the… …is the most important criterion for thermal protection system thickness. This correlation… …determine the required thickness of the forebody thermal protection system for aerocapture and EDL… …using an insulating thermal protection system. The same approach is taken to determining the… 

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APA (6th Edition):

Zinner, E. J. (2019). Assessment of aerocapture-entry trajectories for human Mars exploration. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/104938

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):

Zinner, Evan J. “Assessment of aerocapture-entry trajectories for human Mars exploration.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed March 01, 2021. http://hdl.handle.net/2142/104938.

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

MLA Handbook (7th Edition):

Zinner, Evan J. “Assessment of aerocapture-entry trajectories for human Mars exploration.” 2019. Web. 01 Mar 2021.

Vancouver:

Zinner EJ. Assessment of aerocapture-entry trajectories for human Mars exploration. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2142/104938.

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

Council of Science Editors:

Zinner EJ. Assessment of aerocapture-entry trajectories for human Mars exploration. [Thesis]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/104938

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


Delft University of Technology

29. Clar, Thibault (author). Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft.

Degree: 2019, Delft University of Technology

With the global increase in passenger traffic and growing popularity of long-haul routes over the Asia Pacific region and Atlantic Ocean, the possibility for hypersonic… (more)

Subjects/Keywords: Hypersonic Transport; Multi-Disciplinary Optimisation; Thermal Protection System; Mass estimation; Liquid hydrogen; Hypersonic Engineering Methods; Parametric model; CAD; Automatic meshing; HASA; WAATs; Viscous empirical corrections; PANAIR; Shape Optimisation; Hypersonic engine model

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

APA (6th Edition):

Clar, T. (. (2019). Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2ca126a0-b302-4190-b03d-a9bcf8bed8d4

Chicago Manual of Style (16th Edition):

Clar, Thibault (author). “Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft.” 2019. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:2ca126a0-b302-4190-b03d-a9bcf8bed8d4.

MLA Handbook (7th Edition):

Clar, Thibault (author). “Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft.” 2019. Web. 01 Mar 2021.

Vancouver:

Clar T(. Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:2ca126a0-b302-4190-b03d-a9bcf8bed8d4.

Council of Science Editors:

Clar T(. Development and application of a Multidisciplinary Design Optimisation sizing platform for the conceptual design of hypersonic long-range transport aircraft. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:2ca126a0-b302-4190-b03d-a9bcf8bed8d4

30. Sidor, Adam Thomas. Design and manufacturing of conformal ablative heatshields.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Conformal ablators, first introduced in the early 2000s under the NASA Hypersonics Project, are a type of rigid ablative thermal protection system that uses flexible,… (more)

Subjects/Keywords: Thermal protection system; Heatshield; Heat shield; Materials; Optimization; Manufacturing; Design; Vacuum infusion

…1.3 Classification of thermal protection system materials. . . . . . . . . . . . . 4 1.4… …STF Strain to failure TGA Thermogravimetric analysis TPS Thermal Protection System… …thermal protection system that use flexible, rather than rigid, fibrous substrates. These… …Figure 1.3: Classification of thermal protection system materials. Other classifications can… …protection system (TPS), or heat shield, forms the outermost layer of an entry system… 

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

APA (6th Edition):

Sidor, A. T. (2019). Design and manufacturing of conformal ablative heatshields. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61593

Chicago Manual of Style (16th Edition):

Sidor, Adam Thomas. “Design and manufacturing of conformal ablative heatshields.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/61593.

MLA Handbook (7th Edition):

Sidor, Adam Thomas. “Design and manufacturing of conformal ablative heatshields.” 2019. Web. 01 Mar 2021.

Vancouver:

Sidor AT. Design and manufacturing of conformal ablative heatshields. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/61593.

Council of Science Editors:

Sidor AT. Design and manufacturing of conformal ablative heatshields. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61593

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