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You searched for subject:(Atmospheric Entry). Showing records 1 – 30 of 46 total matches.

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University of Illinois – Urbana-Champaign

1. Zuiker, Nicholas J. Linear covariance analysis of atmospheric entry for sample return mission.

Degree: MS, Aerospace Engineering, 2020, University of Illinois – Urbana-Champaign

 Linear covariance analysis is an uncertainty analysis tool comparable to Monte Carlo analysis; both provide similar statistical information about the performance and uncertainties of a… (more)

Subjects/Keywords: entry; covariance; atmospheric

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APA (6th Edition):

Zuiker, N. J. (2020). Linear covariance analysis of atmospheric entry for sample return mission. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/108540

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):

Zuiker, Nicholas J. “Linear covariance analysis of atmospheric entry for sample return mission.” 2020. Thesis, University of Illinois – Urbana-Champaign. Accessed March 01, 2021. http://hdl.handle.net/2142/108540.

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

MLA Handbook (7th Edition):

Zuiker, Nicholas J. “Linear covariance analysis of atmospheric entry for sample return mission.” 2020. Web. 01 Mar 2021.

Vancouver:

Zuiker NJ. Linear covariance analysis of atmospheric entry for sample return mission. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2020. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2142/108540.

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

Council of Science Editors:

Zuiker NJ. Linear covariance analysis of atmospheric entry for sample return mission. [Thesis]. University of Illinois – Urbana-Champaign; 2020. Available from: http://hdl.handle.net/2142/108540

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


University of Tennessee – Knoxville

2. Brakefield, Braxton Lott. Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth.

Degree: MS, Aerospace Engineering, 2019, University of Tennessee – Knoxville

 The Hercules Single-Stage Reusable Vehicle (HSRV) is an innovative rocket that has been designed for use at Mars. However, with the renewed focus on returning… (more)

Subjects/Keywords: Reentry; Hercules; HSRV; Atmospheric Entry; Spaceflight; Aerocapture

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APA (6th Edition):

Brakefield, B. L. (2019). Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/5521

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):

Brakefield, Braxton Lott. “Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth.” 2019. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/5521.

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

MLA Handbook (7th Edition):

Brakefield, Braxton Lott. “Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth.” 2019. Web. 01 Mar 2021.

Vancouver:

Brakefield BL. Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth. [Internet] [Thesis]. University of Tennessee – Knoxville; 2019. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/5521.

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

Council of Science Editors:

Brakefield BL. Atmospheric Entry Performance of the Hercules Single-Stage Reusable Vehicle at Earth. [Thesis]. University of Tennessee – Knoxville; 2019. Available from: https://trace.tennessee.edu/utk_gradthes/5521

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


Georgia Tech

3. Kutty, Prasad M. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.

Degree: MS, Aerospace Engineering, 2014, Georgia Tech

 The reconstruction of entry, descent and landing (EDL) trajectories is significantly affected by the knowledge of the atmospheric conditions during flight. Away from Earth, this… (more)

Subjects/Keywords: Trajectory reconstruction; Entry, descent and landing; Space vehicles; Space trajectories; Space vehicles Atmospheric entry; Algorithms

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APA (6th Edition):

Kutty, P. M. (2014). Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51893

Chicago Manual of Style (16th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/51893.

MLA Handbook (7th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Web. 01 Mar 2021.

Vancouver:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Internet] [Masters thesis]. Georgia Tech; 2014. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/51893.

Council of Science Editors:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Masters Thesis]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51893


Delft University of Technology

4. Hoogendoorn, R. (author). Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach.

Degree: 2016, Delft University of Technology

Due to the increasing number of space debris objects in orbit around Earth, the need increases for accurate predictions of impact time and location. These… (more)

Subjects/Keywords: Atmospheric entry; Uncertainty propagation; Statistical Impact Prediction; Space Debris; PDF propagation; Atmospheric decay

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APA (6th Edition):

Hoogendoorn, R. (. (2016). Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:161f7ec2-29e7-4eca-91ff-d84e40b053a4

Chicago Manual of Style (16th Edition):

Hoogendoorn, R (author). “Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach.” 2016. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:161f7ec2-29e7-4eca-91ff-d84e40b053a4.

MLA Handbook (7th Edition):

Hoogendoorn, R (author). “Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach.” 2016. Web. 01 Mar 2021.

Vancouver:

Hoogendoorn R(. Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:161f7ec2-29e7-4eca-91ff-d84e40b053a4.

Council of Science Editors:

Hoogendoorn R(. Statistical Impact Prediction of Space Debris: The Uncertainty Propagation Approach. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:161f7ec2-29e7-4eca-91ff-d84e40b053a4

5. Lamet, Jean-Michel. Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows.

Degree: Docteur es, Energétique, 2009, Châtenay-Malabry, Ecole centrale de Paris

Le dimensionnement des protections thermiques des véhicules spatiaux nécessite la connaissance des flux de chaleur à la surface de l'engin. Pour le type de rentrée… (more)

Subjects/Keywords: Rayonnement hors d'équilibre; Modèle de bandes; Atmospheric re-entry; Nonequilibirum radiation; Air plasma

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APA (6th Edition):

Lamet, J. (2009). Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows. (Doctoral Dissertation). Châtenay-Malabry, Ecole centrale de Paris. Retrieved from http://www.theses.fr/2009ECAP0026

Chicago Manual of Style (16th Edition):

Lamet, Jean-Michel. “Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows.” 2009. Doctoral Dissertation, Châtenay-Malabry, Ecole centrale de Paris. Accessed March 01, 2021. http://www.theses.fr/2009ECAP0026.

MLA Handbook (7th Edition):

Lamet, Jean-Michel. “Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows.” 2009. Web. 01 Mar 2021.

Vancouver:

Lamet J. Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows. [Internet] [Doctoral dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2009. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2009ECAP0026.

Council of Science Editors:

Lamet J. Transferts radiatifs dans les écoulements hypersoniques de rentrée atmosphérique terrestre : Radiative transfers in earth atmospheric re-entry's hypersonic flows. [Doctoral Dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2009. Available from: http://www.theses.fr/2009ECAP0026

6. Barka, Lucile. Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry.

Degree: Docteur es, Sciences pour l'ingénieur, 2018, Perpignan

Afin de mieux estimer la survivabilité des débris spatiaux lorsqu’ils retombent sur Terre (masse finale et surface meurtrie), la base de données matériaux du code… (more)

Subjects/Keywords: Rentrée atmosphérique; Débris spatiaux; Oxydation; Émissivité; Atmospheric re-entry; Space debris; Oxidation; Emissivity

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APA (6th Edition):

Barka, L. (2018). Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry. (Doctoral Dissertation). Perpignan. Retrieved from http://www.theses.fr/2018PERP0042

Chicago Manual of Style (16th Edition):

Barka, Lucile. “Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry.” 2018. Doctoral Dissertation, Perpignan. Accessed March 01, 2021. http://www.theses.fr/2018PERP0042.

MLA Handbook (7th Edition):

Barka, Lucile. “Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry.” 2018. Web. 01 Mar 2021.

Vancouver:

Barka L. Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry. [Internet] [Doctoral dissertation]. Perpignan; 2018. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2018PERP0042.

Council of Science Editors:

Barka L. Etude de la survivabilité des débris spatiaux en phase de rentrée atmosphérique (oxydation et émissivité) : Survivability of space debris during their atmospheric re-entry. [Doctoral Dissertation]. Perpignan; 2018. Available from: http://www.theses.fr/2018PERP0042


Delft University of Technology

7. Başkaya, Ata (author). Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications.

Degree: 2020, Delft University of Technology

Atmospheric entry is a crucial phase in planetary exploration missions. During entry, the vehicle experiences severe heating at hypersonic speeds. To ensure the survival of… (more)

Subjects/Keywords: Atmospheric entry; Hypersonics; Gas-surface interactions; Thermal nonequilibrium; Immersed boundary methods; Ablation

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APA (6th Edition):

Başkaya, A. (. (2020). Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1e8866d5-86e4-4879-ac87-022707170eee

Chicago Manual of Style (16th Edition):

Başkaya, Ata (author). “Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications.” 2020. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:1e8866d5-86e4-4879-ac87-022707170eee.

MLA Handbook (7th Edition):

Başkaya, Ata (author). “Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications.” 2020. Web. 01 Mar 2021.

Vancouver:

Başkaya A(. Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:1e8866d5-86e4-4879-ac87-022707170eee.

Council of Science Editors:

Başkaya A(. Coupling of an Immersed Boundary Finite Volume Solver with an Aerothermodynamic Library for Atmospheric Entry Applications. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:1e8866d5-86e4-4879-ac87-022707170eee


University of Kentucky

8. 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

9. Ferrier, Loïc. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.

Degree: Docteur es, Dynamiques des fluides, 2012, Toulouse, ISAE

Quotidiennement, des objets orbitant à proximité de la Terre (ou géocroiseurs) impactent cette dernière. Lorsque la dimension de l'objet atteint une taille critique (autour de… (more)

Subjects/Keywords: Hypersonique; Trajectographie; Aérothermodynamique; Entrée atmosphérique; Géocroiseurs; Rayonnement; Ablation; Fragmentation; Hypersonic; Trajectography; AeroThermoDynamics; Atmospheric Entry; NEOs; Radiation; Ablation; Fragmentation; 532

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APA (6th Edition):

Ferrier, L. (2012). Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2012ESAE0017

Chicago Manual of Style (16th Edition):

Ferrier, Loïc. “Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.” 2012. Doctoral Dissertation, Toulouse, ISAE. Accessed March 01, 2021. http://www.theses.fr/2012ESAE0017.

MLA Handbook (7th Edition):

Ferrier, Loïc. “Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.” 2012. Web. 01 Mar 2021.

Vancouver:

Ferrier L. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2012. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2012ESAE0017.

Council of Science Editors:

Ferrier L. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. [Doctoral Dissertation]. Toulouse, ISAE; 2012. Available from: http://www.theses.fr/2012ESAE0017

10. Prévereaud, Ysolde. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.

Degree: Docteur es, Dynamique des fluides et Energétique et transferts, 2014, Toulouse, ISAE

Afin de déterminer l’état dans lequel les fragments arrivent au sol et leurs points d’impact, une compréhension fine des phénomènes physiques intervenant lors de la… (more)

Subjects/Keywords: Rentrée atmosphérique; Débris spatiaux; Aérothermodynamique; Conduction; Oxydation; Ablation; Atmospheric re-Entry; Space debris; Aerothermodynamics; Conduction; Oxidation; Ablation; 532

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APA (6th Edition):

Prévereaud, Y. (2014). Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2014ESAE0021

Chicago Manual of Style (16th Edition):

Prévereaud, Ysolde. “Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.” 2014. Doctoral Dissertation, Toulouse, ISAE. Accessed March 01, 2021. http://www.theses.fr/2014ESAE0021.

MLA Handbook (7th Edition):

Prévereaud, Ysolde. “Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.” 2014. Web. 01 Mar 2021.

Vancouver:

Prévereaud Y. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2014. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2014ESAE0021.

Council of Science Editors:

Prévereaud Y. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. [Doctoral Dissertation]. Toulouse, ISAE; 2014. Available from: http://www.theses.fr/2014ESAE0021

11. Scoggins, James. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.

Degree: Docteur es, Énergétique, 2017, Université Paris-Saclay (ComUE)

Cette thèse est centrée sur le couplage entre les phénomènes d’écoulement, d’ablation et de rayonnement au voisinage du point d’arrêt de véhicules d’entrée atmosphérique pourvus… (more)

Subjects/Keywords: Entrée atmosphérique; Hypersonique; Aerothermodynamique; Rayonnement; Ablation; Équilibre multiphase; Atmospheric entry; Hypersonics; Aerothermodynamics; Radiation; Ablation; Coupling; Multiphase equilibrium

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APA (6th Edition):

Scoggins, J. (2017). Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. (Doctoral Dissertation). Université Paris-Saclay (ComUE). Retrieved from http://www.theses.fr/2017SACLC048

Chicago Manual of Style (16th Edition):

Scoggins, James. “Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.” 2017. Doctoral Dissertation, Université Paris-Saclay (ComUE). Accessed March 01, 2021. http://www.theses.fr/2017SACLC048.

MLA Handbook (7th Edition):

Scoggins, James. “Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.” 2017. Web. 01 Mar 2021.

Vancouver:

Scoggins J. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. [Internet] [Doctoral dissertation]. Université Paris-Saclay (ComUE); 2017. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2017SACLC048.

Council of Science Editors:

Scoggins J. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. [Doctoral Dissertation]. Université Paris-Saclay (ComUE); 2017. Available from: http://www.theses.fr/2017SACLC048

12. 和泉, 有祐. 大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨).

Degree: 修士(科学), 2017, The University of Tokyo / 東京大学

Subjects/Keywords: Atmospheric Entry; Hypersonic Flow; Aerodynamic Characteristics; Wind Tunnel; Meteorite

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APA (6th Edition):

和泉, . (2017). 大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨). (Thesis). The University of Tokyo / 東京大学. Retrieved from http://hdl.handle.net/2261/48830

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):

和泉, 有祐. “大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨).” 2017. Thesis, The University of Tokyo / 東京大学. Accessed March 01, 2021. http://hdl.handle.net/2261/48830.

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

MLA Handbook (7th Edition):

和泉, 有祐. “大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨).” 2017. Web. 01 Mar 2021.

Vancouver:

和泉 . 大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨). [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2261/48830.

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

Council of Science Editors:

和泉 . 大気圏突入を想定した衝突天体の挙動に関する極超音速空気力学的研究(要旨). [Thesis]. The University of Tokyo / 東京大学; 2017. Available from: http://hdl.handle.net/2261/48830

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


University of Missouri – Columbia

13. McKee, Steven Edward, 1987-. Flight mechanics and control for an unpowered reusable launch vehicle.

Degree: 2011, University of Missouri – Columbia

 A new strategy has been developed to aid in allowing a reusable launch vehicle to complete the Trajectory Area Energy Management (TAEM) phase of reentry.… (more)

Subjects/Keywords: Trajectory Area Energy Management (TAEM); Reusable space vehicles; Launch vehicles (Astronautics); Space vehicles  – Atmospheric entry; Trajectories (Mechanics)

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APA (6th Edition):

McKee, Steven Edward, 1. (2011). Flight mechanics and control for an unpowered reusable launch vehicle. (Thesis). University of Missouri – Columbia. Retrieved from http://hdl.handle.net/10355/11496

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):

McKee, Steven Edward, 1987-. “Flight mechanics and control for an unpowered reusable launch vehicle.” 2011. Thesis, University of Missouri – Columbia. Accessed March 01, 2021. http://hdl.handle.net/10355/11496.

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

MLA Handbook (7th Edition):

McKee, Steven Edward, 1987-. “Flight mechanics and control for an unpowered reusable launch vehicle.” 2011. Web. 01 Mar 2021.

Vancouver:

McKee, Steven Edward 1. Flight mechanics and control for an unpowered reusable launch vehicle. [Internet] [Thesis]. University of Missouri – Columbia; 2011. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10355/11496.

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

Council of Science Editors:

McKee, Steven Edward 1. Flight mechanics and control for an unpowered reusable launch vehicle. [Thesis]. University of Missouri – Columbia; 2011. Available from: http://hdl.handle.net/10355/11496

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


Virginia Tech

14. Baradell, Donald L. Range control during initial phases of supercircular reentries.

Degree: MS, Aerospace Engineering, 1962, Virginia Tech

 For direct reentry from a lunar or deep space mission, considerable variation in reentry plane, reentry point, and reentry angle must be anticipated. The returning… (more)

Subjects/Keywords: LD5655.V855 1962.B373; Space vehicles  – Atmospheric entry

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APA (6th Edition):

Baradell, D. L. (1962). Range control during initial phases of supercircular reentries. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64680

Chicago Manual of Style (16th Edition):

Baradell, Donald L. “Range control during initial phases of supercircular reentries.” 1962. Masters Thesis, Virginia Tech. Accessed March 01, 2021. http://hdl.handle.net/10919/64680.

MLA Handbook (7th Edition):

Baradell, Donald L. “Range control during initial phases of supercircular reentries.” 1962. Web. 01 Mar 2021.

Vancouver:

Baradell DL. Range control during initial phases of supercircular reentries. [Internet] [Masters thesis]. Virginia Tech; 1962. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10919/64680.

Council of Science Editors:

Baradell DL. Range control during initial phases of supercircular reentries. [Masters Thesis]. Virginia Tech; 1962. Available from: http://hdl.handle.net/10919/64680


University of Texas – Austin

15. Dubois-Matra, Olivier. Development of multisensor fusion techniques with gating networks applied to reentry vehicles.

Degree: PhD, Aerospace Engineering, 2003, University of Texas – Austin

 The problem of model inaccuracy for Extended Kalman Filters (EKF) is addressed in the case of vehicle atmospheric entry tracking and navigation with a filter… (more)

Subjects/Keywords: Multisensor data fusion; Space vehicles – Atmospheric entry; Kalman filtering

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APA (6th Edition):

Dubois-Matra, O. (2003). Development of multisensor fusion techniques with gating networks applied to reentry vehicles. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/552

Chicago Manual of Style (16th Edition):

Dubois-Matra, Olivier. “Development of multisensor fusion techniques with gating networks applied to reentry vehicles.” 2003. Doctoral Dissertation, University of Texas – Austin. Accessed March 01, 2021. http://hdl.handle.net/2152/552.

MLA Handbook (7th Edition):

Dubois-Matra, Olivier. “Development of multisensor fusion techniques with gating networks applied to reentry vehicles.” 2003. Web. 01 Mar 2021.

Vancouver:

Dubois-Matra O. Development of multisensor fusion techniques with gating networks applied to reentry vehicles. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2003. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2152/552.

Council of Science Editors:

Dubois-Matra O. Development of multisensor fusion techniques with gating networks applied to reentry vehicles. [Doctoral Dissertation]. University of Texas – Austin; 2003. Available from: http://hdl.handle.net/2152/552


Virginia Tech

16. Gracey, Christopher. Fixed-trim re-entry guidance analysis.

Degree: PhD, Aerospace and Ocean Engineering, 1981, Virginia Tech

 The terminal guidance problem for a fixed-trim re-entry body is formulated with the objective of synthesizing a closed-loop steering law. A transformation of variables is… (more)

Subjects/Keywords: LD5655.V856 1981.G724; Ballistic missiles  – Atmospheric entry

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APA (6th Edition):

Gracey, C. (1981). Fixed-trim re-entry guidance analysis. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71128

Chicago Manual of Style (16th Edition):

Gracey, Christopher. “Fixed-trim re-entry guidance analysis.” 1981. Doctoral Dissertation, Virginia Tech. Accessed March 01, 2021. http://hdl.handle.net/10919/71128.

MLA Handbook (7th Edition):

Gracey, Christopher. “Fixed-trim re-entry guidance analysis.” 1981. Web. 01 Mar 2021.

Vancouver:

Gracey C. Fixed-trim re-entry guidance analysis. [Internet] [Doctoral dissertation]. Virginia Tech; 1981. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10919/71128.

Council of Science Editors:

Gracey C. Fixed-trim re-entry guidance analysis. [Doctoral Dissertation]. Virginia Tech; 1981. Available from: http://hdl.handle.net/10919/71128


University of Kentucky

17. Schroeder, Olivia. Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver.

Degree: 2018, University of Kentucky

 Modeling the atmospheric entry of spacecraft is challenging because of the large number of physical phenomena that occur during the process. In order to study… (more)

Subjects/Keywords: atmospheric entry; thermal protection systems; material response; ablation; arc-jet; Aerodynamics and Fluid Mechanics; Space Vehicles

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APA (6th Edition):

Schroeder, O. (2018). Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/122

Chicago Manual of Style (16th Edition):

Schroeder, Olivia. “Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver.” 2018. Masters Thesis, University of Kentucky. Accessed March 01, 2021. https://uknowledge.uky.edu/me_etds/122.

MLA Handbook (7th Edition):

Schroeder, Olivia. “Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver.” 2018. Web. 01 Mar 2021.

Vancouver:

Schroeder O. Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver. [Internet] [Masters thesis]. University of Kentucky; 2018. [cited 2021 Mar 01]. Available from: https://uknowledge.uky.edu/me_etds/122.

Council of Science Editors:

Schroeder O. Verification and Validation Studies for the KATS Aerothermodynamics and Material Response Solver. [Masters Thesis]. University of Kentucky; 2018. Available from: https://uknowledge.uky.edu/me_etds/122


Texas A&M University

18. Fitzgerald, Steve Matthew. Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Orbital transfer (Space flight); Space vehicles - Atmospheric entry.

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APA (6th Edition):

Fitzgerald, S. M. (2012). Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-F554

Chicago Manual of Style (16th Edition):

Fitzgerald, Steve Matthew. “Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions.” 2012. Masters Thesis, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-F554.

MLA Handbook (7th Edition):

Fitzgerald, Steve Matthew. “Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions.” 2012. Web. 01 Mar 2021.

Vancouver:

Fitzgerald SM. Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-F554.

Council of Science Editors:

Fitzgerald SM. Aeroassisted orbital transfer vehicle guidance performance in the presence of density dispersions. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-F554

19. Lemmer, Kristina Marian. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.

Degree: PhD, Aerospace Engineering, 2009, University of Michigan

 During atmospheric re-entry and hypersonic flight, a bow shock forms around the vehicle leading edge. The air becomes super-heated as it passes through the shock,… (more)

Subjects/Keywords: Helicon Source; Atmospheric Re-entry; Communications Blackout; Aerospace Engineering; Engineering

…7 8 9 11 12 14 16 20 3. Simulating an Atmospheric Re-Entry Plasma . . . . . . . . . . 21… …21 25 27 33 3.5 Summary of Simulating an Atmospheric Re-Entry Plasma . . . . 36 4… …orbiter is not fully encapsulated in plasma during atmospheric re-entry. Due to the shape of the… …communication signals from the Space Shuttle orbiter to Earth during atmospheric re-entry. 2 a… …simulate an atmospheric re-entry plasma in a laboratory setting, and then use crossed electric… 

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APA (6th Edition):

Lemmer, K. M. (2009). Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/63673

Chicago Manual of Style (16th Edition):

Lemmer, Kristina Marian. “Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.” 2009. Doctoral Dissertation, University of Michigan. Accessed March 01, 2021. http://hdl.handle.net/2027.42/63673.

MLA Handbook (7th Edition):

Lemmer, Kristina Marian. “Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System.” 2009. Web. 01 Mar 2021.

Vancouver:

Lemmer KM. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. [Internet] [Doctoral dissertation]. University of Michigan; 2009. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2027.42/63673.

Council of Science Editors:

Lemmer KM. Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System. [Doctoral Dissertation]. University of Michigan; 2009. Available from: http://hdl.handle.net/2027.42/63673


University of Minnesota

20. Gidzak, Vladimyr Mykhalo. A method of simulating fluid structure interactions for deformable decelerators.

Degree: PhD, Aerospace Engineering and Mechanics, 2010, University of Minnesota

 A method is developed for performing simulations that contain fluid-structure interactions between deployable decelerators and a high speed compressible flow. The problem of coupling together… (more)

Subjects/Keywords: Atmospheric Entry; Decelerators; Finite Volume; Fluid Structure Interactions; Aerospace Engineering and Mechanics

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APA (6th Edition):

Gidzak, V. M. (2010). A method of simulating fluid structure interactions for deformable decelerators. (Doctoral Dissertation). University of Minnesota. Retrieved from http://purl.umn.edu/99813

Chicago Manual of Style (16th Edition):

Gidzak, Vladimyr Mykhalo. “A method of simulating fluid structure interactions for deformable decelerators.” 2010. Doctoral Dissertation, University of Minnesota. Accessed March 01, 2021. http://purl.umn.edu/99813.

MLA Handbook (7th Edition):

Gidzak, Vladimyr Mykhalo. “A method of simulating fluid structure interactions for deformable decelerators.” 2010. Web. 01 Mar 2021.

Vancouver:

Gidzak VM. A method of simulating fluid structure interactions for deformable decelerators. [Internet] [Doctoral dissertation]. University of Minnesota; 2010. [cited 2021 Mar 01]. Available from: http://purl.umn.edu/99813.

Council of Science Editors:

Gidzak VM. A method of simulating fluid structure interactions for deformable decelerators. [Doctoral Dissertation]. University of Minnesota; 2010. Available from: http://purl.umn.edu/99813


University of Oklahoma

21. Ling, Lisa. High-fidelity modeling and impact footprint prediction for vehicle breakup analysis.

Degree: PhD, School of Aerospace and Mechanical Engineering, 2005, University of Oklahoma

 For decades, vehicle breakup analysis had been performed for space missions that used nuclear heater or power units in order to assess aerospace nuclear safety… (more)

Subjects/Keywords: Space vehicles Atmospheric entry.; Space vehicles Nuclear power plants.; Engineering, Aerospace.

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APA (6th Edition):

Ling, L. (2005). High-fidelity modeling and impact footprint prediction for vehicle breakup analysis. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/910

Chicago Manual of Style (16th Edition):

Ling, Lisa. “High-fidelity modeling and impact footprint prediction for vehicle breakup analysis.” 2005. Doctoral Dissertation, University of Oklahoma. Accessed March 01, 2021. http://hdl.handle.net/11244/910.

MLA Handbook (7th Edition):

Ling, Lisa. “High-fidelity modeling and impact footprint prediction for vehicle breakup analysis.” 2005. Web. 01 Mar 2021.

Vancouver:

Ling L. High-fidelity modeling and impact footprint prediction for vehicle breakup analysis. [Internet] [Doctoral dissertation]. University of Oklahoma; 2005. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/11244/910.

Council of Science Editors:

Ling L. High-fidelity modeling and impact footprint prediction for vehicle breakup analysis. [Doctoral Dissertation]. University of Oklahoma; 2005. Available from: http://hdl.handle.net/11244/910


University of Kentucky

22. 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

23. 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


Virginia Tech

24. Kim, Moo Do. Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter.

Degree: PhD, Aerospace Engineering, 1983, Virginia Tech

Subjects/Keywords: LD5655.V856 1983.K55; Reusable space vehicles; Space vehicles  – Atmospheric entry; Viscous flow

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APA (6th Edition):

Kim, M. D. (1983). Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/101292

Chicago Manual of Style (16th Edition):

Kim, Moo Do. “Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter.” 1983. Doctoral Dissertation, Virginia Tech. Accessed March 01, 2021. http://hdl.handle.net/10919/101292.

MLA Handbook (7th Edition):

Kim, Moo Do. “Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter.” 1983. Web. 01 Mar 2021.

Vancouver:

Kim MD. Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter. [Internet] [Doctoral dissertation]. Virginia Tech; 1983. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10919/101292.

Council of Science Editors:

Kim MD. Three-dimensional nonequilibrium viscous shock-layer flow over the space shuttle orbiter. [Doctoral Dissertation]. Virginia Tech; 1983. Available from: http://hdl.handle.net/10919/101292

25. Korzun, Ashley Marie. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Supersonic deceleration has been identified as a critical deficiency in extending heritage technologies to the high-mass systems required to achieve long-term exploration goals at Mars.… (more)

Subjects/Keywords: EDL; Planetary entry; Mars exploration; Retropropulsion; Opposing jets; Aerodynamics; Space vehicles Atmospheric entry; Space vehicles Atmospheric entry Mars (Planet); Aeronautics; Mars (Planet) Aeronautics

…39 2 Entry masses (kg) for a 10 m-diameter, 70-deg sphere-cone aeroshell. 62… …5 4 Simplified flowfield over a blunt body entry vehicle [3]… …Salas’ approach with experimental data for contoured nozzles exhausting into an atmospheric… …Disk-Gap-Band DOE Design of Experiments DOF Degree of Freedom EDL Entry, Descent, and… …Landing EDL-SA Entry, Descent, and Landing Systems Analysis xxii EFF Exploration Feed… 

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APA (6th Edition):

Korzun, A. M. (2012). Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43667

Chicago Manual of Style (16th Edition):

Korzun, Ashley Marie. “Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.” 2012. Doctoral Dissertation, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/43667.

MLA Handbook (7th Edition):

Korzun, Ashley Marie. “Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.” 2012. Web. 01 Mar 2021.

Vancouver:

Korzun AM. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/43667.

Council of Science Editors:

Korzun AM. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43667

26. Wagner, John Joseph. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Many modern entry guidance systems depend on predictions of atmospheric parameters, notably atmospheric density, in order to guide the entry vehicle to some desired final… (more)

Subjects/Keywords: Atmospheric density prediction; Entry vehicle guidance; Ensemble forecasting; Atmospheric density estimator

…prior to arrival. Many entry vehicles, however, rely on knowledge of atmospheric properties… …uncertainty associated with many common atmospheric density estimators may allow guided entry… …thereby permits the entry system to counteract greater levels of atmospheric density uncertainty… …however, knowledge of the atmospheric properties can be improved, guided entry systems would be… …atmospheric density on the entry trajectory will diminish with altitude. For aerocapture, the… 

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APA (6th Edition):

Wagner, J. J. (2014). An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53046

Chicago Manual of Style (16th Edition):

Wagner, John Joseph. “An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/53046.

MLA Handbook (7th Edition):

Wagner, John Joseph. “An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.” 2014. Web. 01 Mar 2021.

Vancouver:

Wagner JJ. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/53046.

Council of Science Editors:

Wagner JJ. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53046

27. Mahzari, Milad. Inverse estimation methodology for the analysis of aeroheating and thermal protection system data.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Thermal Protection System (TPS) is required to shield an atmospheric entry vehicle against the high surface heating environment experienced during hypersonic flight. There are significant… (more)

Subjects/Keywords: Inverse problems; Thermal protection system; Aerothermodynamics; Ablative materials; Parameter estimation; Atmospheric entry; Space vehicles Shielding (Heat); Shielding (Heat); Space vehicles Atmospheric entry; Space vehicles Materials

…of a blunt body’s aerothermal environment during atmospheric entry… …MEADS Mars Entry Atmospheric Data System MEDLI MSL Entry, Descent, and Landing… …sensors, called Mars Entry Atmospheric Data System (MEADS) and temperature sensors… …during a blunt body’s atmospheric entry. Computational Fluid Dynam- Figure 4: Schematic of a… …blunt body’s aerothermal environment during atmospheric entry. ics (CFD) tools are… 

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APA (6th Edition):

Mahzari, M. (2013). Inverse estimation methodology for the analysis of aeroheating and thermal protection system data. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50327

Chicago Manual of Style (16th Edition):

Mahzari, Milad. “Inverse estimation methodology for the analysis of aeroheating and thermal protection system data.” 2013. Doctoral Dissertation, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/50327.

MLA Handbook (7th Edition):

Mahzari, Milad. “Inverse estimation methodology for the analysis of aeroheating and thermal protection system data.” 2013. Web. 01 Mar 2021.

Vancouver:

Mahzari M. Inverse estimation methodology for the analysis of aeroheating and thermal protection system data. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/50327.

Council of Science Editors:

Mahzari M. Inverse estimation methodology for the analysis of aeroheating and thermal protection system data. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50327

28. Coumar, Sandra. Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries.

Degree: Docteur es, Physique, 2017, Université d'Orléans

Ces dernières années, les missions spatiales bénéficient d'un regain d'intérêt. Cependant, lorsqu’arrive laphase d’entrée dans l’atmosphère, nous faisons encore face à d’importantes difficultés. Afin de… (more)

Subjects/Keywords: Gaz et Plasmas; Ingénierie spatiale; Décharge luminescente; (R)entrée atmosphérique; Hyper/supersonique; Aérodynamique; Décharge pulsée; Ecoulement raréfié; Déséquilibre thermique; Gas and Plasma Physics, Aerospace engineering; EDL technique, Glow discharge; Atmospheric (re-)entry; Hypersonic; Supersonic; Aerodynamics; Pulsed discharge; Rarefied flow; Thermal disequilibrium

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

APA (6th Edition):

Coumar, S. (2017). Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries. (Doctoral Dissertation). Université d'Orléans. Retrieved from http://www.theses.fr/2017ORLE2025

Chicago Manual of Style (16th Edition):

Coumar, Sandra. “Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries.” 2017. Doctoral Dissertation, Université d'Orléans. Accessed March 01, 2021. http://www.theses.fr/2017ORLE2025.

MLA Handbook (7th Edition):

Coumar, Sandra. “Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries.” 2017. Web. 01 Mar 2021.

Vancouver:

Coumar S. Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries. [Internet] [Doctoral dissertation]. Université d'Orléans; 2017. [cited 2021 Mar 01]. Available from: http://www.theses.fr/2017ORLE2025.

Council of Science Editors:

Coumar S. Etude des mécanismes physiques induits pas un actionneur plasma appliqué au contrôle d’écoulements raréfiés super/hypersoniques dans le cadre de rentrées atmosphériques : Study of physical mechanisms induced by a plasma actuator for super/hypersonic rarefied flows applied to atmospheric entries. [Doctoral Dissertation]. Université d'Orléans; 2017. Available from: http://www.theses.fr/2017ORLE2025


Texas A&M University

29. Green, Derek Scott. A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Space vehicles - Atmospheric entry.; Orbital transfer (Space flight); Vibration (Aeronautics)

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

APA (6th Edition):

Green, D. S. (2012). A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1991-THESIS-G795

Chicago Manual of Style (16th Edition):

Green, Derek Scott. “A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime.” 2012. Masters Thesis, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1991-THESIS-G795.

MLA Handbook (7th Edition):

Green, Derek Scott. “A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime.” 2012. Web. 01 Mar 2021.

Vancouver:

Green DS. A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1991-THESIS-G795.

Council of Science Editors:

Green DS. A comparative study of vibrational relaxation models for the aeroassisted orbital transfer vehicle flight regime. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1991-THESIS-G795


Texas A&M University

30. Koteshwar, Rajeev. A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Space flight to Mars.; Space vehicles - Atmospheric entry.; Space vehicles - Vibration.

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

APA (6th Edition):

Koteshwar, R. (2012). A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-K87

Chicago Manual of Style (16th Edition):

Koteshwar, Rajeev. “A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle.” 2012. Masters Thesis, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-K87.

MLA Handbook (7th Edition):

Koteshwar, Rajeev. “A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle.” 2012. Web. 01 Mar 2021.

Vancouver:

Koteshwar R. A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-K87.

Council of Science Editors:

Koteshwar R. A comparative study of vibrational relaxation and chemical reaction models for the Martian entry vehicle. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1992-THESIS-K87

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