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You searched for subject:(Re entry Vehicle). Showing records 1 – 6 of 6 total matches.

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University of Missouri – Columbia

1. Bryan, Josiah A. Maximum-range trajectories for an unpowered reusable launch vehicle.

Degree: 2011, University of Missouri – Columbia

 A software package has been developed that numerically maximizes the range of an unpowered reusable launch vehicle (RLV) during the Terminal Area Energy Management (TAEM)… (more)

Subjects/Keywords: terminal area energy management; trajectory optimization; unpowered re-entry; quasi-equilibrium glide; reusable launch vehicle

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

APA (6th Edition):

Bryan, J. A. (2011). Maximum-range trajectories for an unpowered reusable launch vehicle. (Thesis). University of Missouri – Columbia. Retrieved from http://hdl.handle.net/10355/14529

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):

Bryan, Josiah A. “Maximum-range trajectories for an unpowered reusable launch vehicle.” 2011. Thesis, University of Missouri – Columbia. Accessed March 01, 2021. http://hdl.handle.net/10355/14529.

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

MLA Handbook (7th Edition):

Bryan, Josiah A. “Maximum-range trajectories for an unpowered reusable launch vehicle.” 2011. Web. 01 Mar 2021.

Vancouver:

Bryan JA. Maximum-range trajectories for an unpowered reusable launch vehicle. [Internet] [Thesis]. University of Missouri – Columbia; 2011. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10355/14529.

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

Council of Science Editors:

Bryan JA. Maximum-range trajectories for an unpowered reusable launch vehicle. [Thesis]. University of Missouri – Columbia; 2011. Available from: http://hdl.handle.net/10355/14529

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


University of Kentucky

2. 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


Delft University of Technology

3. De Ridder, S. (author). Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area.

Degree: 2009, Delft University of Technology

The unpowered entry of a winged re-entry vehicle, such as the HORUS-2B, consists of a hypersonic atmospheric re-entry phase, a Terminal Area Energy Management (TAEM)… (more)

Subjects/Keywords: TAEM; genetic algorithm; Energy management; winged re-entry vehicle; optimal trajectories

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APA (6th Edition):

De Ridder, S. (. (2009). Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5e801af7-b006-478d-8b13-3f6f55ecff6a

Chicago Manual of Style (16th Edition):

De Ridder, S (author). “Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area.” 2009. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:5e801af7-b006-478d-8b13-3f6f55ecff6a.

MLA Handbook (7th Edition):

De Ridder, S (author). “Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area.” 2009. Web. 01 Mar 2021.

Vancouver:

De Ridder S(. Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area. [Internet] [Masters thesis]. Delft University of Technology; 2009. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:5e801af7-b006-478d-8b13-3f6f55ecff6a.

Council of Science Editors:

De Ridder S(. Study on optimal Trajectories and Energy Management Capabilities of a Winged Re-Entry Vehicle during the Terminal Area. [Masters Thesis]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:5e801af7-b006-478d-8b13-3f6f55ecff6a


University of Kentucky

4. 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

5. Perumal, Raja Pandi. Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules.

Degree: 2016, Luleå University of Technology

As humanity gobbles up the available natural resources to satisfy the growing energy demands, an impending need for an alternate source of valuable commodity… (more)

Subjects/Keywords: Technology; Asteroid Mining; Re-entry; Trajectory Design; Mission Design; Vehicle Design; Teknik

…rate . . . . . . . . . . . Hayabusa Re-entry Vehicle [4]… …Stresses on the RV (Stresses are expressed in N/m2 ) . . . . Re-entry Vehicle model… …vehicle . . . . . . . . . . . . . . . . . . . Deceleration Profile of the re-entry vehicle… …Heat Flux experienced by the re-entry vehicle . . . . . . . . . . . . . . Illustration of… …Line Vehicle Design Considerations . . . . . . . . . . . . . . . . . . Re-entry Vehicle… 

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

APA (6th Edition):

Perumal, R. P. (2016). Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52177

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):

Perumal, Raja Pandi. “Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules.” 2016. Thesis, Luleå University of Technology. Accessed March 01, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52177.

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

MLA Handbook (7th Edition):

Perumal, Raja Pandi. “Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules.” 2016. Web. 01 Mar 2021.

Vancouver:

Perumal RP. Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2021 Mar 01]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52177.

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

Council of Science Editors:

Perumal RP. Return Trajectories and Re-Entry Requirements for Mining Transporter Capsules. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-52177

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


Indian Institute of Science

6. Arora, Rajesh Kumar. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.

Degree: PhD, Faculty of Engineering, 2009, Indian Institute of Science

 Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Under broad heading of these methods, numerous algorithms such as collocation,… (more)

Subjects/Keywords: Genetic Algorithm; Spacecraft - Trajectory Optimization; Reusable Launch Vehicle (RLV); On-line Trajectory-Reshaping Algorithm; Trajectory Dispersion; Trajectory Optimization; Trajectory Design; Re-entry Vehicles; Chebyshev Polynomials; Astronautics

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

APA (6th Edition):

Arora, R. K. (2009). Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/424

Chicago Manual of Style (16th Edition):

Arora, Rajesh Kumar. “Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.” 2009. Doctoral Dissertation, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/424.

MLA Handbook (7th Edition):

Arora, Rajesh Kumar. “Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission.” 2009. Web. 01 Mar 2021.

Vancouver:

Arora RK. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2009. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/424.

Council of Science Editors:

Arora RK. Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission. [Doctoral Dissertation]. Indian Institute of Science; 2009. Available from: http://etd.iisc.ac.in/handle/2005/424

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