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You searched for subject:(orbital debris). Showing records 1 – 30 of 35 total matches.

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Georgia Tech

1. Long, Alexandra Cheryl. Passively stable pyramid sail to deorbit small satellites.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

Orbital debris is a growing problem in low-Earth orbit, especially with a number of commercial companies intending to launch hundreds to thousands of micro-satellites into… (more)

Subjects/Keywords: Orbital debris; Deorbit stategies; Drag sail

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APA (6th Edition):

Long, A. C. (2018). Passively stable pyramid sail to deorbit small satellites. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60269

Chicago Manual of Style (16th Edition):

Long, Alexandra Cheryl. “Passively stable pyramid sail to deorbit small satellites.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 23, 2021. http://hdl.handle.net/1853/60269.

MLA Handbook (7th Edition):

Long, Alexandra Cheryl. “Passively stable pyramid sail to deorbit small satellites.” 2018. Web. 23 Jan 2021.

Vancouver:

Long AC. Passively stable pyramid sail to deorbit small satellites. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1853/60269.

Council of Science Editors:

Long AC. Passively stable pyramid sail to deorbit small satellites. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60269


Virginia Tech

2. Thurber, Andrew. Investigations of Hypervelocity Impact Physics.

Degree: PhD, Mechanical Engineering, 2014, Virginia Tech

 Spacecraft and satellites in orbit are under an increasing threat of impact from orbital debris and naturally occurring meteoroids. While objects larger than 10 cm… (more)

Subjects/Keywords: impact; orbital debris; finite element; shock physics

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APA (6th Edition):

Thurber, A. (2014). Investigations of Hypervelocity Impact Physics. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95298

Chicago Manual of Style (16th Edition):

Thurber, Andrew. “Investigations of Hypervelocity Impact Physics.” 2014. Doctoral Dissertation, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/95298.

MLA Handbook (7th Edition):

Thurber, Andrew. “Investigations of Hypervelocity Impact Physics.” 2014. Web. 23 Jan 2021.

Vancouver:

Thurber A. Investigations of Hypervelocity Impact Physics. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/95298.

Council of Science Editors:

Thurber A. Investigations of Hypervelocity Impact Physics. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/95298


University of Colorado

3. Anderson, Paul V. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.

Degree: PhD, Aerospace Engineering Sciences, 2010, University of Colorado

  The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming increasingly contaminated with orbital debris, but is heavily populated… (more)

Subjects/Keywords: active debris removal; geostationary orbit; geosynchronous orbit; orbital debris; Aerospace Engineering

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APA (6th Edition):

Anderson, P. V. (2010). Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/14

Chicago Manual of Style (16th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Doctoral Dissertation, University of Colorado. Accessed January 23, 2021. https://scholar.colorado.edu/asen_gradetds/14.

MLA Handbook (7th Edition):

Anderson, Paul V. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2010. Web. 23 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2021 Jan 23]. Available from: https://scholar.colorado.edu/asen_gradetds/14.

Council of Science Editors:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/14


University of Colorado

4. Anderson, Paul Vincent. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming increasingly contaminated with orbital debris, but is heavily populated… (more)

Subjects/Keywords: active debris removal; geostationary orbit; geosynchronous orbit; orbital debris; Aerospace Engineering

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APA (6th Edition):

Anderson, P. V. (2015). Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/91

Chicago Manual of Style (16th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 23, 2021. https://scholar.colorado.edu/asen_gradetds/91.

MLA Handbook (7th Edition):

Anderson, Paul Vincent. “Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime.” 2015. Web. 23 Jan 2021.

Vancouver:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2021 Jan 23]. Available from: https://scholar.colorado.edu/asen_gradetds/91.

Council of Science Editors:

Anderson PV. Characterizing Longitude-Dependent Orbital Debris Congestion in the Geosynchronous Orbit Regime. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/91


University of Colorado

5. Jasper, Lee E.Z. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.

Degree: PhD, Aerospace Engineering Sciences, 2014, University of Colorado

  Towing objects in space has become an increasingly researched mission concept. Active debris removal, satellite servicing, and asteroid retrieval concepts in many cases rely… (more)

Subjects/Keywords: active debris removal; input shaping; orbital debris; space tether; tethered towing; Aerospace Engineering

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APA (6th Edition):

Jasper, L. E. Z. (2014). Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/82

Chicago Manual of Style (16th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Doctoral Dissertation, University of Colorado. Accessed January 23, 2021. https://scholar.colorado.edu/asen_gradetds/82.

MLA Handbook (7th Edition):

Jasper, Lee E Z. “Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects.” 2014. Web. 23 Jan 2021.

Vancouver:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Internet] [Doctoral dissertation]. University of Colorado; 2014. [cited 2021 Jan 23]. Available from: https://scholar.colorado.edu/asen_gradetds/82.

Council of Science Editors:

Jasper LEZ. Open-Loop Thrust Profile Development for Tethered Towing of Large Space Objects. [Doctoral Dissertation]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/82


University of Manitoba

6. Cherniaev, Aleksandr. Design and analysis of orbital debris protection for spacecraft composite pressure vessels.

Degree: Mechanical Engineering, 2016, University of Manitoba

 Being parts of spacecraft systems, composite overwrapped pressure vessels (COPVs) are exposed to orbital debris environment. In the case of impact of orbital debris on… (more)

Subjects/Keywords: Orbital debris; Composite pressure vessel; Hypervelocity impact; Impact shielding; Impact modeling

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APA (6th Edition):

Cherniaev, A. (2016). Design and analysis of orbital debris protection for spacecraft composite pressure vessels. (Thesis). University of Manitoba. Retrieved from http://hdl.handle.net/1993/31949

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):

Cherniaev, Aleksandr. “Design and analysis of orbital debris protection for spacecraft composite pressure vessels.” 2016. Thesis, University of Manitoba. Accessed January 23, 2021. http://hdl.handle.net/1993/31949.

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

MLA Handbook (7th Edition):

Cherniaev, Aleksandr. “Design and analysis of orbital debris protection for spacecraft composite pressure vessels.” 2016. Web. 23 Jan 2021.

Vancouver:

Cherniaev A. Design and analysis of orbital debris protection for spacecraft composite pressure vessels. [Internet] [Thesis]. University of Manitoba; 2016. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1993/31949.

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

Council of Science Editors:

Cherniaev A. Design and analysis of orbital debris protection for spacecraft composite pressure vessels. [Thesis]. University of Manitoba; 2016. Available from: http://hdl.handle.net/1993/31949

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


University of Toronto

7. Hakima, Houman. A New Approach to Active Removal of Space Debris.

Degree: PhD, 2020, University of Toronto

 As a result of human space activities for over sixty years, there exist numerous man-made debris objects in the Earth orbits. Such objects not only… (more)

Subjects/Keywords: Active Debris Removal; Attitude and Orbit Control; Attitude Dynamics; Deorbiter CubeSat; Orbital Dynamics; Space Debris; 0538

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APA (6th Edition):

Hakima, H. (2020). A New Approach to Active Removal of Space Debris. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/101359

Chicago Manual of Style (16th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Doctoral Dissertation, University of Toronto. Accessed January 23, 2021. http://hdl.handle.net/1807/101359.

MLA Handbook (7th Edition):

Hakima, Houman. “A New Approach to Active Removal of Space Debris.” 2020. Web. 23 Jan 2021.

Vancouver:

Hakima H. A New Approach to Active Removal of Space Debris. [Internet] [Doctoral dissertation]. University of Toronto; 2020. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1807/101359.

Council of Science Editors:

Hakima H. A New Approach to Active Removal of Space Debris. [Doctoral Dissertation]. University of Toronto; 2020. Available from: http://hdl.handle.net/1807/101359

8. O'Gorman, John. The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit.

Degree: MS, Public Policy (CLA), 2018, Rochester Institute of Technology

  Ever since the launch of Sputnik in 1957, humans have put over 40,000 pieces of debris into orbit around the Earth. In particular, most… (more)

Subjects/Keywords: Debris; LEO; Orbital; Space; Sustainability

…infrastructure, an increasing number of launches and competing interests makes 7 orbital debris a… …region because it is the most economical to reach. Therefore, most orbital debris is… …42,000 km which is also of interest to debris studies because of its unique orbital period of… …to mitigate the creation and effects of orbital debris [to the FCC]" (… …control of the hazards of orbital debris is reassuring, but not enough to solve the problem of… 

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APA (6th Edition):

O'Gorman, J. (2018). The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/9796

Chicago Manual of Style (16th Edition):

O'Gorman, John. “The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit.” 2018. Masters Thesis, Rochester Institute of Technology. Accessed January 23, 2021. https://scholarworks.rit.edu/theses/9796.

MLA Handbook (7th Edition):

O'Gorman, John. “The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit.” 2018. Web. 23 Jan 2021.

Vancouver:

O'Gorman J. The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit. [Internet] [Masters thesis]. Rochester Institute of Technology; 2018. [cited 2021 Jan 23]. Available from: https://scholarworks.rit.edu/theses/9796.

Council of Science Editors:

O'Gorman J. The Cost of Clean Space- A Study of the Additional Fuel Costs of Launching Above Low Earth Orbit. [Masters Thesis]. Rochester Institute of Technology; 2018. Available from: https://scholarworks.rit.edu/theses/9796


Penn State University

9. McTernan, Jesse Kane. DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS .

Degree: 2011, Penn State University

 Electrodynamic tethers can be used to harvest energy onboard a spacecraft orbiting the Earth or any planetary body with a magnetic field and surrounding plasma.… (more)

Subjects/Keywords: debris mitigation; orbital energy; enrgy harvesting; energy; space tether; electrodynamic tether; propulsion

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APA (6th Edition):

McTernan, J. K. (2011). DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12063

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):

McTernan, Jesse Kane. “DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS .” 2011. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/12063.

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

MLA Handbook (7th Edition):

McTernan, Jesse Kane. “DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS .” 2011. Web. 23 Jan 2021.

Vancouver:

McTernan JK. DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/12063.

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

Council of Science Editors:

McTernan JK. DEVELOPMENT OF A MODELING CAPABILITY FOR ENERGY HARVESTING MODULES IN ELECTRODYNAMIC TETHER SYSTEMS . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/12063

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


University of Toronto

10. Cotten, Scott Bradley. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.

Degree: 2014, University of Toronto

In the context of space debris mitigation, a major challenge currently facing the space community is the removal of nano and microsatellites from orbit following… (more)

Subjects/Keywords: Magnetic Attitude Control; Microsatellite Technology; Orbital Debris; Spacecraft Deorbiting; Thermal Control of Space Systems; 0538

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APA (6th Edition):

Cotten, S. B. (2014). Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/68553

Chicago Manual of Style (16th Edition):

Cotten, Scott Bradley. “Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.” 2014. Masters Thesis, University of Toronto. Accessed January 23, 2021. http://hdl.handle.net/1807/68553.

MLA Handbook (7th Edition):

Cotten, Scott Bradley. “Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission.” 2014. Web. 23 Jan 2021.

Vancouver:

Cotten SB. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1807/68553.

Council of Science Editors:

Cotten SB. Design, Analysis, Implementation, and Testing of the Thermal Control, and Attitude Determination and Control Systems for the CanX-7 Nanosatellite Mission. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/68553


University of Colorado

11. Bennett, Trevor John. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.

Degree: PhD, 2017, University of Colorado

  In recent years, there is a growing interest in active debris removal and on-orbit servicing of Earth orbiting assets. The growing need for such… (more)

Subjects/Keywords: contactless/touchless; electrostatic actuation; formation flying; orbital debris; relative navigation; Aerospace Engineering; Physics

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APA (6th Edition):

Bennett, T. J. (2017). On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/226

Chicago Manual of Style (16th Edition):

Bennett, Trevor John. “On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.” 2017. Doctoral Dissertation, University of Colorado. Accessed January 23, 2021. https://scholar.colorado.edu/asen_gradetds/226.

MLA Handbook (7th Edition):

Bennett, Trevor John. “On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries.” 2017. Web. 23 Jan 2021.

Vancouver:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Jan 23]. Available from: https://scholar.colorado.edu/asen_gradetds/226.

Council of Science Editors:

Bennett TJ. On-Orbit 3-Dimensional Electrostatic Detumble for Generic Spacecraft Geometries. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/226


University of Manitoba

12. Jones, Alexander James Bryan. Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection.

Degree: Mechanical Engineering, 2018, University of Manitoba

 Many commonly-used orbits are increasingly cluttered with orbital debris, posing a significant threat to space assets, which require enhanced protection. Recent studies demonstrate that foam-core… (more)

Subjects/Keywords: Orbital debris; Numerical modelling; Metal foam core; Hypervelocity impact; Autodyn; MMOD; HVI

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APA (6th Edition):

Jones, A. J. B. (2018). Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection. (Masters Thesis). University of Manitoba. Retrieved from http://hdl.handle.net/1993/32882

Chicago Manual of Style (16th Edition):

Jones, Alexander James Bryan. “Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection.” 2018. Masters Thesis, University of Manitoba. Accessed January 23, 2021. http://hdl.handle.net/1993/32882.

MLA Handbook (7th Edition):

Jones, Alexander James Bryan. “Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection.” 2018. Web. 23 Jan 2021.

Vancouver:

Jones AJB. Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection. [Internet] [Masters thesis]. University of Manitoba; 2018. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1993/32882.

Council of Science Editors:

Jones AJB. Modelling of hypervelocity impact on foam-core sandwich panel with enhanced capability for orbital debris protection. [Masters Thesis]. University of Manitoba; 2018. Available from: http://hdl.handle.net/1993/32882


University of Toronto

13. Bazzocchi, Michael Christopher Francesco. Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization.

Degree: PhD, 2018, University of Toronto

 In this thesis, an overall framework is established for the redirection of near-Earth asteroids using spacecraft formation strategies in order to access and utilize asteroid… (more)

Subjects/Keywords: Asteroid Redirection; Formation Control; Orbital Dynamics; Spacecraft Formation; Space Debris; Transfer Trajectory Design; 0538

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APA (6th Edition):

Bazzocchi, M. C. F. (2018). Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/89883

Chicago Manual of Style (16th Edition):

Bazzocchi, Michael Christopher Francesco. “Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization.” 2018. Doctoral Dissertation, University of Toronto. Accessed January 23, 2021. http://hdl.handle.net/1807/89883.

MLA Handbook (7th Edition):

Bazzocchi, Michael Christopher Francesco. “Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization.” 2018. Web. 23 Jan 2021.

Vancouver:

Bazzocchi MCF. Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization. [Internet] [Doctoral dissertation]. University of Toronto; 2018. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1807/89883.

Council of Science Editors:

Bazzocchi MCF. Spacecraft Formation Approach to Asteroid Redirection for Resource Utilization. [Doctoral Dissertation]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/89883


Cal Poly

14. Hawkins, Robert A, Jr. Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  There is an increased need for spacecraft to quickly and efficiently de-orbit themselves as the amount of debris in orbit around Earth grows. Defunct… (more)

Subjects/Keywords: CubeSat; de-orbit; orbital debris; drag; orbit; Gossamer; Astrodynamics; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Hawkins, Robert A, J. (2013). Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1139 ; 10.15368/theses.2013.219

Chicago Manual of Style (16th Edition):

Hawkins, Robert A, Jr. “Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats.” 2013. Masters Thesis, Cal Poly. Accessed January 23, 2021. https://digitalcommons.calpoly.edu/theses/1139 ; 10.15368/theses.2013.219.

MLA Handbook (7th Edition):

Hawkins, Robert A, Jr. “Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats.” 2013. Web. 23 Jan 2021.

Vancouver:

Hawkins, Robert A J. Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2021 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/1139 ; 10.15368/theses.2013.219.

Council of Science Editors:

Hawkins, Robert A J. Analysis of an Inflatable Gossamer Device to Efficiently De-Orbit CubeSats. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1139 ; 10.15368/theses.2013.219

15. Horn, Adam Charles. A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation.

Degree: MS, Mechanical & Aerospace Engineering, 2017, Old Dominion University

  The United Nations Inter-Agency Debris Coordination Committee has adopted a 25-year post-mission lifetime requirement for any satellite orbiting below 2000 km in order to… (more)

Subjects/Keywords: CubeSat; Drag brake; Inflatable; Orbital debris; Space; Sublimation; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Horn, A. C. (2017). A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation. (Thesis). Old Dominion University. Retrieved from 9780355409376 ; https://digitalcommons.odu.edu/mae_etds/28

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):

Horn, Adam Charles. “A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation.” 2017. Thesis, Old Dominion University. Accessed January 23, 2021. 9780355409376 ; https://digitalcommons.odu.edu/mae_etds/28.

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

MLA Handbook (7th Edition):

Horn, Adam Charles. “A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation.” 2017. Web. 23 Jan 2021.

Vancouver:

Horn AC. A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation. [Internet] [Thesis]. Old Dominion University; 2017. [cited 2021 Jan 23]. Available from: 9780355409376 ; https://digitalcommons.odu.edu/mae_etds/28.

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

Council of Science Editors:

Horn AC. A Low Cost Inflatable CubeSat Drag Brake Utilizing Sublimation. [Thesis]. Old Dominion University; 2017. Available from: 9780355409376 ; https://digitalcommons.odu.edu/mae_etds/28

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

16. Hofsteenge, R. (author). Computational Methods for the Long-Term Propagation of Space Debris Orbits.

Degree: 2013, Delft University of Technology

Space debris poses a significant problem for the space sector. This problem relates to potential collisions of debris objects with active satellites, which in many… (more)

Subjects/Keywords: space debris; astrodynamics; numerical integration; orbital perturbations

…regions generally have very long orbital lifetimes. Simulating the orbits of debris objects over… …long-term orbital developments of debris objects in graveyard orbits will be considered in… …or orbital debris has been defined by the Inter-Agency Space Debris Coordination Committee… …for the future of spaceflight. 2.3 The Space Debris Environment The higher the orbital… …Figure 2.2. As can be seen in the figure, most orbital debris resides within 2,000 km of the… 

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

APA (6th Edition):

Hofsteenge, R. (. (2013). Computational Methods for the Long-Term Propagation of Space Debris Orbits. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:eee70164-4c99-470d-b8ee-5314ffcf63f8

Chicago Manual of Style (16th Edition):

Hofsteenge, R (author). “Computational Methods for the Long-Term Propagation of Space Debris Orbits.” 2013. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:eee70164-4c99-470d-b8ee-5314ffcf63f8.

MLA Handbook (7th Edition):

Hofsteenge, R (author). “Computational Methods for the Long-Term Propagation of Space Debris Orbits.” 2013. Web. 23 Jan 2021.

Vancouver:

Hofsteenge R(. Computational Methods for the Long-Term Propagation of Space Debris Orbits. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:eee70164-4c99-470d-b8ee-5314ffcf63f8.

Council of Science Editors:

Hofsteenge R(. Computational Methods for the Long-Term Propagation of Space Debris Orbits. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:eee70164-4c99-470d-b8ee-5314ffcf63f8


Cal Poly

17. Biehl, James Patrick. FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

  The main purpose of this thesis is to develop a search strategy for space debris that are in the geosynchronous orbit (GEO) region. The… (more)

Subjects/Keywords: Space Debris; Search Strategies; Orbits; Orbital Dynamics

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APA (6th Edition):

Biehl, J. P. (2010). FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/355 ; 10.15368/theses.2010.124

Chicago Manual of Style (16th Edition):

Biehl, James Patrick. “FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO.” 2010. Masters Thesis, Cal Poly. Accessed January 23, 2021. https://digitalcommons.calpoly.edu/theses/355 ; 10.15368/theses.2010.124.

MLA Handbook (7th Edition):

Biehl, James Patrick. “FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO.” 2010. Web. 23 Jan 2021.

Vancouver:

Biehl JP. FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2021 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/355 ; 10.15368/theses.2010.124.

Council of Science Editors:

Biehl JP. FORMULATION OF A SEARCH STRATEGY FOR SPACE DEBRIS AT GEO. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/355 ; 10.15368/theses.2010.124


Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

18. Skoulidou, Despoina. Dynamical evolution of artificial satellites and space debris in near earth region.

Degree: 2019, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ)

In this study, we perform a complete, dynamical cartography of the dynamics of satellites and space debris in the near Earth space, by using detailed… (more)

Subjects/Keywords: Τροχιακή μηχανική; Τεχνητοί δορυφόροι; Διαστημικά κατάλοιπα; Εγγύς διαστημικό περιβάλλον; Orbital mechanics; Artificial satellites; Space debris; Near earth space environment

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APA (6th Edition):

Skoulidou, D. (2019). Dynamical evolution of artificial satellites and space debris in near earth region. (Thesis). Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Retrieved from http://hdl.handle.net/10442/hedi/46490

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):

Skoulidou, Despoina. “Dynamical evolution of artificial satellites and space debris in near earth region.” 2019. Thesis, Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ). Accessed January 23, 2021. http://hdl.handle.net/10442/hedi/46490.

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

MLA Handbook (7th Edition):

Skoulidou, Despoina. “Dynamical evolution of artificial satellites and space debris in near earth region.” 2019. Web. 23 Jan 2021.

Vancouver:

Skoulidou D. Dynamical evolution of artificial satellites and space debris in near earth region. [Internet] [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10442/hedi/46490.

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

Council of Science Editors:

Skoulidou D. Dynamical evolution of artificial satellites and space debris in near earth region. [Thesis]. Aristotle University Of Thessaloniki (AUTH); Αριστοτέλειο Πανεπιστήμιο Θεσσαλονίκης (ΑΠΘ); 2019. Available from: http://hdl.handle.net/10442/hedi/46490

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

19. Diaz, Christina R. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  This thesis will present the effects of the orbital debris evolution in two key areas: the geosynchronous disposal orbit regime known as “graveyard” and… (more)

Subjects/Keywords: orbital debris; debris; collisions; ODPO; orbital mechanics; fortran; Astrodynamics; Other Aerospace Engineering

debris is a present and future hazard to all Earth space operations. Orbital debris consists of… …collisions also contribute to the present population. Orbital debris’ time in orbit is dependent on… …the orbital altitude. Debris in lower orbits often reenter within several years to decades… …GEO Region Understanding debris evolution requires a thorough understanding of the orbital… …to orbital debris, geopotential wells are of interest due to their interesting behavior and… 

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APA (6th Edition):

Diaz, C. R. (2013). A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157

Chicago Manual of Style (16th Edition):

Diaz, Christina R. “A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.” 2013. Masters Thesis, Cal Poly. Accessed January 23, 2021. https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157.

MLA Handbook (7th Edition):

Diaz, Christina R. “A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS.” 2013. Web. 23 Jan 2021.

Vancouver:

Diaz CR. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2021 Jan 23]. Available from: https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157.

Council of Science Editors:

Diaz CR. A STUDY OF THE COLLISIONAL EVOLUTION OF ORBITAL DEBRIS IN GEOPOTENTIAL WELLS AND GEO DISPOSAL ORBITS. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1063 ; 10.15368/theses.2013.157


University of Florida

20. Cojuangco, Ai-Ai Lumnay C. Orbital Lifetime Analyses of Pico- and Nano-Satellites.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 In recent years, orbital debris has been a growing concern for the space industry due to its potential risk of causing collisions. Several agencies and… (more)

Subjects/Keywords: Altitude; Artificial satellites; Atmospheric density; Drag coefficient; Orbital elements; Orbital lifetime; Orbitals; Orbits; Simulations; Space debris; lifetime, nano, orbital, pico, satellite

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APA (6th Edition):

Cojuangco, A. L. C. (2007). Orbital Lifetime Analyses of Pico- and Nano-Satellites. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0020154

Chicago Manual of Style (16th Edition):

Cojuangco, Ai-Ai Lumnay C. “Orbital Lifetime Analyses of Pico- and Nano-Satellites.” 2007. Masters Thesis, University of Florida. Accessed January 23, 2021. https://ufdc.ufl.edu/UFE0020154.

MLA Handbook (7th Edition):

Cojuangco, Ai-Ai Lumnay C. “Orbital Lifetime Analyses of Pico- and Nano-Satellites.” 2007. Web. 23 Jan 2021.

Vancouver:

Cojuangco ALC. Orbital Lifetime Analyses of Pico- and Nano-Satellites. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2021 Jan 23]. Available from: https://ufdc.ufl.edu/UFE0020154.

Council of Science Editors:

Cojuangco ALC. Orbital Lifetime Analyses of Pico- and Nano-Satellites. [Masters Thesis]. University of Florida; 2007. Available from: https://ufdc.ufl.edu/UFE0020154

21. Deloo, J.A.F. (author). Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination.

Degree: 2015, Delft University of Technology

The aim of this thesis is to investigate a debris-remediation technique where a chaser performs a rendezvous with the debris, establishes a rigid-link connection, and… (more)

Subjects/Keywords: e.deorbit; ENVISAT; Clean Space; Orbital Debris; Uncooperative Rendezvous; Debris Remediation; Safety; Communication; Illumination; Active Debris Removal

…135 Bibliography 139 Appendices 141 A Disturbance Torques and Relative Orbital… …143 A-2 Relative Orbital Perturbations… …in Noordwijk, The Netherlands), where I worked on an active debris-removal mission… …The topic of active debris removal is one that I have found intriguing since the start of my… …students, a heavy space debris removal system. Next, I continued working on the subject during my… 

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APA (6th Edition):

Deloo, J. A. F. (. (2015). Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7f445d54-c758-45a8-b87e-a9c0eec61617

Chicago Manual of Style (16th Edition):

Deloo, J A F (author). “Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:7f445d54-c758-45a8-b87e-a9c0eec61617.

MLA Handbook (7th Edition):

Deloo, J A F (author). “Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination.” 2015. Web. 23 Jan 2021.

Vancouver:

Deloo JAF(. Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:7f445d54-c758-45a8-b87e-a9c0eec61617.

Council of Science Editors:

Deloo JAF(. Analysis of the Rendezvous Phase of e.deorbit: Guidance, Communication and Illumination. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:7f445d54-c758-45a8-b87e-a9c0eec61617

22. Rosenkvist, Kajsa Eriksson. Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers.

Degree: Space Technology, 2019, Luleå University of Technology

  Overcrowding of the Low Earth Orbit (LEO) region is a growing problem. Decades of treating this part of space like a scrap yard has… (more)

Subjects/Keywords: Laser; Orbital; Debris; Removal; Aerospace Engineering; Rymd- och flygteknik

…an informed decision on how the orbital debris problem can be handled. 2 Chapter 2… …system and orbital debris, the media can not be changed. Instead it is vital to choose a… …turbulence divergence angle [m] Debris ~ag Cm d ηc F~g J~ md ν o p~ ρ ~v v [J… …efficiency factor gravitational force impulse debris mass true anomaly angular displacement from… …detonated after disconnection, leaving a much lager amount of debris. A number of satellites have… 

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APA (6th Edition):

Rosenkvist, K. E. (2019). Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77103

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):

Rosenkvist, Kajsa Eriksson. “Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers.” 2019. Thesis, Luleå University of Technology. Accessed January 23, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77103.

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

MLA Handbook (7th Edition):

Rosenkvist, Kajsa Eriksson. “Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers.” 2019. Web. 23 Jan 2021.

Vancouver:

Rosenkvist KE. Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers. [Internet] [Thesis]. Luleå University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77103.

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

Council of Science Editors:

Rosenkvist KE. Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers. [Thesis]. Luleå University of Technology; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77103

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


University of Florida

23. Werremeyer, Mark R. Design of Subsystems for a Representative Modern LEO Satellite.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 This thesis discusses the design of subsystems for a representative modern low Earth Orbit (LEO) satellite. Specifically, the subsystems presented were designed for inclusion on… (more)

Subjects/Keywords: Aluminum; Artificial satellites; Composite materials; Low earth orbits; Magnetism; Nadir; Plumbing; Propulsion; Satellite design; Thrusters; attitude  – debris  – debrisat  – hypervelocity  – impact  – leo  – modern  – orbital  – propulsion  – representative  – satellite  – structure  – subsystems  – test  – thermal

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APA (6th Edition):

Werremeyer, M. R. (2013). Design of Subsystems for a Representative Modern LEO Satellite. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0045534

Chicago Manual of Style (16th Edition):

Werremeyer, Mark R. “Design of Subsystems for a Representative Modern LEO Satellite.” 2013. Masters Thesis, University of Florida. Accessed January 23, 2021. https://ufdc.ufl.edu/UFE0045534.

MLA Handbook (7th Edition):

Werremeyer, Mark R. “Design of Subsystems for a Representative Modern LEO Satellite.” 2013. Web. 23 Jan 2021.

Vancouver:

Werremeyer MR. Design of Subsystems for a Representative Modern LEO Satellite. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2021 Jan 23]. Available from: https://ufdc.ufl.edu/UFE0045534.

Council of Science Editors:

Werremeyer MR. Design of Subsystems for a Representative Modern LEO Satellite. [Masters Thesis]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0045534

24. Maury, Thibaut. Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie.

Degree: Docteur es, Génie des Procédés, 2019, Bordeaux

 L’analyse de cycle de vie environnementale (ACV), d’après l’ISO 14040/44, a été identifiée par l’agence spatiale Européenne, ArianeGroup et plusieurs acteurs de l’industrie spatiale européenne… (more)

Subjects/Keywords: Analyse du Cycle de Vie; Fin de vie; Débris spatiaux; Impact environnemental; Life Cycle Assessment; Environmental impact; Space debris; Orbital space use; Post-Mission Disposal

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APA (6th Edition):

Maury, T. (2019). Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie. (Doctoral Dissertation). Bordeaux. Retrieved from http://www.theses.fr/2019BORD0051

Chicago Manual of Style (16th Edition):

Maury, Thibaut. “Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie.” 2019. Doctoral Dissertation, Bordeaux. Accessed January 23, 2021. http://www.theses.fr/2019BORD0051.

MLA Handbook (7th Edition):

Maury, Thibaut. “Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie.” 2019. Web. 23 Jan 2021.

Vancouver:

Maury T. Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie. [Internet] [Doctoral dissertation]. Bordeaux; 2019. [cited 2021 Jan 23]. Available from: http://www.theses.fr/2019BORD0051.

Council of Science Editors:

Maury T. Consideration of space debris in the life cycle assessment framework : Considération des débris spatiaux dans le cadre de l’analyse de cycle de vie. [Doctoral Dissertation]. Bordeaux; 2019. Available from: http://www.theses.fr/2019BORD0051

25. Van Cor, Jared D. Characterizing Resident Space Object Earthshine Signature Variability.

Degree: MS, Chester F. Carlson Center for Imaging Science (COS), 2017, Rochester Institute of Technology

  There are three major sources of illumination on objects in the near Earth space environment: Sunshine, Moonshine, and Earthshine. For objects in this environment… (more)

Subjects/Keywords: DIRSIG; Earthshine; Earthshine simulation; Orbital debris; Resident space object; Space debris

…Autonomous Telescope mdpt mid point MEO Mid Earth Orbit MODEST Michigan Orbital Debris Survey… …this threat, NASA’s Orbital Debris Program office has placed great emphasis on obtaining… …0.61m aperture Michigan Orbital Debris Survey Telescope (MODEST) in Chili to help… …of countries with space assets reaching 60 and growing, the amount of debris and potential… …Earth shadowing, and near Earth orbital speeds. This problem is compounded by bidirectional… 

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APA (6th Edition):

Van Cor, J. D. (2017). Characterizing Resident Space Object Earthshine Signature Variability. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/9485

Chicago Manual of Style (16th Edition):

Van Cor, Jared D. “Characterizing Resident Space Object Earthshine Signature Variability.” 2017. Masters Thesis, Rochester Institute of Technology. Accessed January 23, 2021. https://scholarworks.rit.edu/theses/9485.

MLA Handbook (7th Edition):

Van Cor, Jared D. “Characterizing Resident Space Object Earthshine Signature Variability.” 2017. Web. 23 Jan 2021.

Vancouver:

Van Cor JD. Characterizing Resident Space Object Earthshine Signature Variability. [Internet] [Masters thesis]. Rochester Institute of Technology; 2017. [cited 2021 Jan 23]. Available from: https://scholarworks.rit.edu/theses/9485.

Council of Science Editors:

Van Cor JD. Characterizing Resident Space Object Earthshine Signature Variability. [Masters Thesis]. Rochester Institute of Technology; 2017. Available from: https://scholarworks.rit.edu/theses/9485

26. Roberts, Lyle Edward. Internally Sensed Optical Phased Arrays .

Degree: 2016, Australian National University

 The performance of existing ground-based space debris laser ranging systems can be improved by directing more light onto space debris by coherently combining multiple lasers… (more)

Subjects/Keywords: Optical Phased Arrays; Control Systems; Lasers; Optics; Stabilisation; Stabilization; Coherent Beam Combining; Space Debris; Orbital Debris; Interferometry; Digitally Enhanced Heterodyne Interferometry; Phasemeters; Digitally Implemented Phasemeters; Field Programmable Gate Array; FPGA; OPA; CBC; Internal sensing; Internally sensed

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APA (6th Edition):

Roberts, L. E. (2016). Internally Sensed Optical Phased Arrays . (Thesis). Australian National University. Retrieved from http://hdl.handle.net/1885/110523

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):

Roberts, Lyle Edward. “Internally Sensed Optical Phased Arrays .” 2016. Thesis, Australian National University. Accessed January 23, 2021. http://hdl.handle.net/1885/110523.

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

MLA Handbook (7th Edition):

Roberts, Lyle Edward. “Internally Sensed Optical Phased Arrays .” 2016. Web. 23 Jan 2021.

Vancouver:

Roberts LE. Internally Sensed Optical Phased Arrays . [Internet] [Thesis]. Australian National University; 2016. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1885/110523.

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

Council of Science Editors:

Roberts LE. Internally Sensed Optical Phased Arrays . [Thesis]. Australian National University; 2016. Available from: http://hdl.handle.net/1885/110523

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


University of Colorado

27. Trowbridge, Michael Aaron. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.

Degree: MS, Aerospace Engineering Sciences, 2014, University of Colorado

  A software prototype for autonomous 3D scanning of uncooperatively rotating orbital debris using a point cloud sensor is designed and tested. The software successfully… (more)

Subjects/Keywords: 3D scanning; explicit loop closure heuristic; Graph SLAM; model generation; orbital debris; point clouds; Aerospace Engineering; Artificial Intelligence and Robotics; Computer-Aided Engineering and Design; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Trowbridge, M. A. (2014). Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/86

Chicago Manual of Style (16th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Masters Thesis, University of Colorado. Accessed January 23, 2021. https://scholar.colorado.edu/asen_gradetds/86.

MLA Handbook (7th Edition):

Trowbridge, Michael Aaron. “Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors.” 2014. Web. 23 Jan 2021.

Vancouver:

Trowbridge MA. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. [Internet] [Masters thesis]. University of Colorado; 2014. [cited 2021 Jan 23]. Available from: https://scholar.colorado.edu/asen_gradetds/86.

Council of Science Editors:

Trowbridge MA. Autonomous 3D Model Generation of Orbital Debris using Point Cloud Sensors. [Masters Thesis]. University of Colorado; 2014. Available from: https://scholar.colorado.edu/asen_gradetds/86

28. Mackay, Sean Leland. Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change.

Degree: PhD, Earth & Environment, 2016, Boston University

 Antarctic debris-covered glaciers are potential archives of long-term climate change. However, the geomorphic response of these systems to climate forcing is not well understood. To… (more)

Subjects/Keywords: Geomorphology; Antarctica; Climate change; Cosmogenic nuclide dating; Debris-covered glacier; Ground-penetrating radar; Orbital forcing

…1 Chapter 2: Cold-based debris-covered glaciers: evaluating their potential as climate… …paced late Pleistocene climate change recorded in the structure of Antarctic debris-covered… …35 Figure 2.6. Measured air, supraglacial debris, and ice temperatures at selected… …Figure 2.16. Morphometric properties of supraglacial debris on Mullins Glacier ...........67… …Figure 2.17. Sedimentological variation in supraglacial debris on Mullins Glacier .........71… 

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APA (6th Edition):

Mackay, S. L. (2016). Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change. (Doctoral Dissertation). Boston University. Retrieved from http://hdl.handle.net/2144/14508

Chicago Manual of Style (16th Edition):

Mackay, Sean Leland. “Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change.” 2016. Doctoral Dissertation, Boston University. Accessed January 23, 2021. http://hdl.handle.net/2144/14508.

MLA Handbook (7th Edition):

Mackay, Sean Leland. “Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change.” 2016. Web. 23 Jan 2021.

Vancouver:

Mackay SL. Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change. [Internet] [Doctoral dissertation]. Boston University; 2016. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/2144/14508.

Council of Science Editors:

Mackay SL. Age, origin and evolution of Antarctic debris-covered glaciers: implications for landscape evolution and long-term climate change. [Doctoral Dissertation]. Boston University; 2016. Available from: http://hdl.handle.net/2144/14508


University of Florida

29. Wyatt, Mark C., 1972-. Signatures of planets in the observable structure of circumstellar debris disks.

Degree: PhD, Astronomy, 1999, University of Florida

Subjects/Keywords: Asymmetry; Debris disks; Orbital eccentricity; Orbits; Particle collisions; Particle density; Particle emission; Particle resonance; Planets; Zodiacal cloud; Circumstellar matter

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

APA (6th Edition):

Wyatt, Mark C., 1. (1999). Signatures of planets in the observable structure of circumstellar debris disks. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/AA00040505

Chicago Manual of Style (16th Edition):

Wyatt, Mark C., 1972-. “Signatures of planets in the observable structure of circumstellar debris disks.” 1999. Doctoral Dissertation, University of Florida. Accessed January 23, 2021. https://ufdc.ufl.edu/AA00040505.

MLA Handbook (7th Edition):

Wyatt, Mark C., 1972-. “Signatures of planets in the observable structure of circumstellar debris disks.” 1999. Web. 23 Jan 2021.

Vancouver:

Wyatt, Mark C. 1. Signatures of planets in the observable structure of circumstellar debris disks. [Internet] [Doctoral dissertation]. University of Florida; 1999. [cited 2021 Jan 23]. Available from: https://ufdc.ufl.edu/AA00040505.

Council of Science Editors:

Wyatt, Mark C. 1. Signatures of planets in the observable structure of circumstellar debris disks. [Doctoral Dissertation]. University of Florida; 1999. Available from: https://ufdc.ufl.edu/AA00040505


Indian Institute of Science

30. Anilkumar, A K. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.

Degree: PhD, Faculty of Engineering, 2005, Indian Institute of Science

 In the space surrounding the earth there are two major regions where orbital debris causes concern. They are the Low Earth Orbits (LEO) up to… (more)

Subjects/Keywords: Aerospace Engineering; Space Debris Modelling; On Orbit Breakup; Debris Clouds; Evolution; Collision Risk; Re entry; Kalman Filter; ASSEMBLE Model; SIMPLE model; Orbital Elements; Propagation; Collision probability; Semi major axis

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

APA (6th Edition):

Anilkumar, A. K. (2005). NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/80

Chicago Manual of Style (16th Edition):

Anilkumar, A K. “NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.” 2005. Doctoral Dissertation, Indian Institute of Science. Accessed January 23, 2021. http://etd.iisc.ac.in/handle/2005/80.

MLA Handbook (7th Edition):

Anilkumar, A K. “NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS.” 2005. Web. 23 Jan 2021.

Vancouver:

Anilkumar AK. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2005. [cited 2021 Jan 23]. Available from: http://etd.iisc.ac.in/handle/2005/80.

Council of Science Editors:

Anilkumar AK. NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS. [Doctoral Dissertation]. Indian Institute of Science; 2005. Available from: http://etd.iisc.ac.in/handle/2005/80

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