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You searched for subject:(Spacecraft). Showing records 1 – 30 of 377 total matches.

[1] [2] [3] [4] [5] … [13]

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McGill University

1. Hill, Steven Michael. The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space.

Degree: Master of Laws, Institute of Air and Space Law, 1982, McGill University

Note:

Since the launching of the first COMSAT communications satellite in the early 1960's, there has been an increasing commitment of capital and technology to… (more)

Subjects/Keywords: Spacecraft

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APA (6th Edition):

Hill, S. M. (1982). The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile155693.pdf

Chicago Manual of Style (16th Edition):

Hill, Steven Michael. “The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space.” 1982. Masters Thesis, McGill University. Accessed June 20, 2019. http://digitool.library.mcgill.ca/thesisfile155693.pdf.

MLA Handbook (7th Edition):

Hill, Steven Michael. “The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space.” 1982. Web. 20 Jun 2019.

Vancouver:

Hill SM. The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space. [Internet] [Masters thesis]. McGill University; 1982. [cited 2019 Jun 20]. Available from: http://digitool.library.mcgill.ca/thesisfile155693.pdf.

Council of Science Editors:

Hill SM. The Launch and Insurance of Spacecraft: The Pragmatics of Doing Business in Space. [Masters Thesis]. McGill University; 1982. Available from: http://digitool.library.mcgill.ca/thesisfile155693.pdf


Cornell University

2. Manchester, Zachary. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .

Degree: 2015, Cornell University

 The rise of the consumer electronics industry has led to a profusion of ever smaller, cheaper, and more capable devices, from sensors to computers to… (more)

Subjects/Keywords: Small Spacecraft; Spacecraft Dynamics; Space Systems

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APA (6th Edition):

Manchester, Z. (2015). Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/41055

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):

Manchester, Zachary. “Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .” 2015. Thesis, Cornell University. Accessed June 20, 2019. http://hdl.handle.net/1813/41055.

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

MLA Handbook (7th Edition):

Manchester, Zachary. “Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment .” 2015. Web. 20 Jun 2019.

Vancouver:

Manchester Z. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . [Internet] [Thesis]. Cornell University; 2015. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1813/41055.

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

Council of Science Editors:

Manchester Z. Centimeter-Scale Spacecraft: Design, Fabrication, And Deployment . [Thesis]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/41055

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


Cornell University

3. Reinhardt, Benjamin. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .

Degree: 2015, Cornell University

 Induction couplers exploit eddy-current effects to create force and torque on a target without mechanical contact. Nearly all spacecraft structures include conductive material, so induction… (more)

Subjects/Keywords: Spacecraft; Robotics; Electromagnetism

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APA (6th Edition):

Reinhardt, B. (2015). Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/40607

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):

Reinhardt, Benjamin. “Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .” 2015. Thesis, Cornell University. Accessed June 20, 2019. http://hdl.handle.net/1813/40607.

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

MLA Handbook (7th Edition):

Reinhardt, Benjamin. “Induction Couplers: Contactless On-Orbit Actuation For Space Robotics .” 2015. Web. 20 Jun 2019.

Vancouver:

Reinhardt B. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . [Internet] [Thesis]. Cornell University; 2015. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1813/40607.

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

Council of Science Editors:

Reinhardt B. Induction Couplers: Contactless On-Orbit Actuation For Space Robotics . [Thesis]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40607

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


University of Southern California

4. Reddy, Shalini A. Control of spacecraft with flexible structures using pulse-modulated thrusters.

Degree: PhD, Mechanical Engineering, 2012, University of Southern California

 A methodology for the design of robust control systems for flexible spacecraft undergoing a large angle maneuver using pulse-modulated thrusters is proposed. The need for… (more)

Subjects/Keywords: spacecraft; dynamics; control

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APA (6th Edition):

Reddy, S. A. (2012). Control of spacecraft with flexible structures using pulse-modulated thrusters. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1638

Chicago Manual of Style (16th Edition):

Reddy, Shalini A. “Control of spacecraft with flexible structures using pulse-modulated thrusters.” 2012. Doctoral Dissertation, University of Southern California. Accessed June 20, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1638.

MLA Handbook (7th Edition):

Reddy, Shalini A. “Control of spacecraft with flexible structures using pulse-modulated thrusters.” 2012. Web. 20 Jun 2019.

Vancouver:

Reddy SA. Control of spacecraft with flexible structures using pulse-modulated thrusters. [Internet] [Doctoral dissertation]. University of Southern California; 2012. [cited 2019 Jun 20]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1638.

Council of Science Editors:

Reddy SA. Control of spacecraft with flexible structures using pulse-modulated thrusters. [Doctoral Dissertation]. University of Southern California; 2012. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/84663/rec/1638

5. Pande, Seetesh. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.

Degree: Aerospace Engineering, 2013, University of Petroleum and Energy Studies (UPES)

Abstract avalible

References p.116 - 120 and Appendix p.121 - 129

Advisors/Committee Members: Ugur, Guven.

Subjects/Keywords: Spacecraft; Stellar

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APA (6th Edition):

Pande, S. (2013). Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. (Thesis). University of Petroleum and Energy Studies (UPES). Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/41384

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):

Pande, Seetesh. “Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.” 2013. Thesis, University of Petroleum and Energy Studies (UPES). Accessed June 20, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/41384.

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

MLA Handbook (7th Edition):

Pande, Seetesh. “Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -.” 2013. Web. 20 Jun 2019.

Vancouver:

Pande S. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. [Internet] [Thesis]. University of Petroleum and Energy Studies (UPES); 2013. [cited 2019 Jun 20]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/41384.

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

Council of Science Editors:

Pande S. Analysis of spacecraft trajectories on the polar axis over the event horizon of a stellar originated rotating kerr black hole; -. [Thesis]. University of Petroleum and Energy Studies (UPES); 2013. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/41384

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


University of Toronto

6. Bonin, Grant. Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft.

Degree: 2009, University of Toronto

The development of a multi-mission small spacecraft power system is described. This system has been designed for the University of Toronto Space Flight Laboratory Generic… (more)

Subjects/Keywords: Spacecraft; Power Systems; 0538

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APA (6th Edition):

Bonin, G. (2009). Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/18940

Chicago Manual of Style (16th Edition):

Bonin, Grant. “Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft.” 2009. Masters Thesis, University of Toronto. Accessed June 20, 2019. http://hdl.handle.net/1807/18940.

MLA Handbook (7th Edition):

Bonin, Grant. “Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft.” 2009. Web. 20 Jun 2019.

Vancouver:

Bonin G. Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft. [Internet] [Masters thesis]. University of Toronto; 2009. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1807/18940.

Council of Science Editors:

Bonin G. Power System Design, Analysis, and Power Electronics Implementation on Generic Nanosatellite Bus (GNB) Spacecraft. [Masters Thesis]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/18940


Delft University of Technology

7. Kuiper, J.M. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.

Degree: 2012, Delft University of Technology

 Mass-spring and liquid dampers enable structural vibration control to attenuate single, coupled lateral and torsional vibrations in diverse structures. Out of these, the passively tuned… (more)

Subjects/Keywords: Spacecraft ADCS

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APA (6th Edition):

Kuiper, J. M. (2012). Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60

Chicago Manual of Style (16th Edition):

Kuiper, J M. “Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.” 2012. Doctoral Dissertation, Delft University of Technology. Accessed June 20, 2019. http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60.

MLA Handbook (7th Edition):

Kuiper, J M. “Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures.” 2012. Web. 20 Jun 2019.

Vancouver:

Kuiper JM. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. [Internet] [Doctoral dissertation]. Delft University of Technology; 2012. [cited 2019 Jun 20]. Available from: http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60.

Council of Science Editors:

Kuiper JM. Broadband Liquid Dampers to Stabilize Flexible Spacecraft Structures. [Doctoral Dissertation]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; urn:NBN:nl:ui:24-uuid:680a3181-2062-4923-be05-2c16ee1efa60 ; http://resolver.tudelft.nl/uuid:680a3181-2062-4923-be05-2c16ee1efa60


Cornell University

8. McLoughlin, Terence Hugh. SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS .

Degree: 2008, Cornell University

 Future NASA missions requiring spacecraft formation flying require an extremely high level of autonomy and robustness when compared to single spacecraft systems. This is especially… (more)

Subjects/Keywords: spacecraft; formation; estimation; optimization; scheduling

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APA (6th Edition):

McLoughlin, T. H. (2008). SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/11588

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):

McLoughlin, Terence Hugh. “SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS .” 2008. Thesis, Cornell University. Accessed June 20, 2019. http://hdl.handle.net/1813/11588.

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

MLA Handbook (7th Edition):

McLoughlin, Terence Hugh. “SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS .” 2008. Web. 20 Jun 2019.

Vancouver:

McLoughlin TH. SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS . [Internet] [Thesis]. Cornell University; 2008. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1813/11588.

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

Council of Science Editors:

McLoughlin TH. SCALABLE DECENTRALIZED NAVIGATION AND CONTROL ALGORITHMS FOR LARGE SCALE SPACECRAFT FORMATIONS . [Thesis]. Cornell University; 2008. Available from: http://hdl.handle.net/1813/11588

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


Delft University of Technology

9. Ragupathy, A.P. Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:.

Degree: 2016, Delft University of Technology

 Accurate thermal characterisation of composite structures can help structural designers in predicting thermal paths in a spacecraft structure and assessing the effect of modifying materials… (more)

Subjects/Keywords: thermal; composites; spacecraft; FEM

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APA (6th Edition):

Ragupathy, A. P. (2016). Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:273a0318-d8be-4448-b4e2-310a4c6a297a

Chicago Manual of Style (16th Edition):

Ragupathy, A P. “Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:.” 2016. Masters Thesis, Delft University of Technology. Accessed June 20, 2019. http://resolver.tudelft.nl/uuid:273a0318-d8be-4448-b4e2-310a4c6a297a.

MLA Handbook (7th Edition):

Ragupathy, A P. “Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:.” 2016. Web. 20 Jun 2019.

Vancouver:

Ragupathy AP. Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Jun 20]. Available from: http://resolver.tudelft.nl/uuid:273a0318-d8be-4448-b4e2-310a4c6a297a.

Council of Science Editors:

Ragupathy AP. Thermal Characterization of Structure-Integrated Thermal Subsystems based on the MASCOT Landing Module:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:273a0318-d8be-4448-b4e2-310a4c6a297a


University of Texas – Austin

10. Christian, John Allen. Optical navigation for a spacecraft in a planetary system.

Degree: Aerospace Engineering and Engineering Mechanics, 2010, University of Texas – Austin

 Recent years have seen ambitious robotic exploration missions to other planets and a renewed interest in sending humans beyond low Earth orbit. These activities give… (more)

Subjects/Keywords: Spacecraft; Optical navigation; Attitude filtering

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APA (6th Edition):

Christian, J. A. (2010). Optical navigation for a spacecraft in a planetary system. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-05-829

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):

Christian, John Allen. “Optical navigation for a spacecraft in a planetary system.” 2010. Thesis, University of Texas – Austin. Accessed June 20, 2019. http://hdl.handle.net/2152/ETD-UT-2010-05-829.

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

MLA Handbook (7th Edition):

Christian, John Allen. “Optical navigation for a spacecraft in a planetary system.” 2010. Web. 20 Jun 2019.

Vancouver:

Christian JA. Optical navigation for a spacecraft in a planetary system. [Internet] [Thesis]. University of Texas – Austin; 2010. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-829.

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

Council of Science Editors:

Christian JA. Optical navigation for a spacecraft in a planetary system. [Thesis]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-829

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


University of Colorado

11. Stiles, Laura Ann. Electrostatic In ation of Membrane Space Structures.

Degree: PhD, Aerospace Engineering Sciences, 2013, University of Colorado

  Membrane space structures provide a lightweight and cost effective alternative to traditional mechanical systems. The low-mass and high deployed-to-stored volume ratios allow for larger… (more)

Subjects/Keywords: Deployable Spacecraft; Inflatable Structures; Plasma Physics; Spacecraft Charging; Aerospace Engineering

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APA (6th Edition):

Stiles, L. A. (2013). Electrostatic In ation of Membrane Space Structures. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/92

Chicago Manual of Style (16th Edition):

Stiles, Laura Ann. “Electrostatic In ation of Membrane Space Structures.” 2013. Doctoral Dissertation, University of Colorado. Accessed June 20, 2019. http://scholar.colorado.edu/asen_gradetds/92.

MLA Handbook (7th Edition):

Stiles, Laura Ann. “Electrostatic In ation of Membrane Space Structures.” 2013. Web. 20 Jun 2019.

Vancouver:

Stiles LA. Electrostatic In ation of Membrane Space Structures. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Jun 20]. Available from: http://scholar.colorado.edu/asen_gradetds/92.

Council of Science Editors:

Stiles LA. Electrostatic In ation of Membrane Space Structures. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/92


Georgia Tech

12. Francis, Parker. Development of the evolved common hardware bus (TECHBus).

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

 This thesis presents the design and analysis of a small spacecraft bus for use by the Georgia Tech Space Systems Design Lab. It is designed… (more)

Subjects/Keywords: Spacecraft design; Spacecraft bus; Reliability; CubeSat; Nanosatellite; Small satellite

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APA (6th Edition):

Francis, P. (2016). Development of the evolved common hardware bus (TECHBus). (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55671

Chicago Manual of Style (16th Edition):

Francis, Parker. “Development of the evolved common hardware bus (TECHBus).” 2016. Masters Thesis, Georgia Tech. Accessed June 20, 2019. http://hdl.handle.net/1853/55671.

MLA Handbook (7th Edition):

Francis, Parker. “Development of the evolved common hardware bus (TECHBus).” 2016. Web. 20 Jun 2019.

Vancouver:

Francis P. Development of the evolved common hardware bus (TECHBus). [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1853/55671.

Council of Science Editors:

Francis P. Development of the evolved common hardware bus (TECHBus). [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55671


Penn State University

13. Muncks, John P. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 In this thesis, a process to identify cost-efficient tracking solutions for interplanetary missions is presented. The process is flexible enough to be used in a… (more)

Subjects/Keywords: interplanetary spacecraft; spacecraft tracking; cost-efficient; Deep Space Network

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APA (6th Edition):

Muncks, J. P. (2014). Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23702

Chicago Manual of Style (16th Edition):

Muncks, John P. “Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.” 2014. Masters Thesis, Penn State University. Accessed June 20, 2019. https://etda.libraries.psu.edu/catalog/23702.

MLA Handbook (7th Edition):

Muncks, John P. “Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft.” 2014. Web. 20 Jun 2019.

Vancouver:

Muncks JP. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Jun 20]. Available from: https://etda.libraries.psu.edu/catalog/23702.

Council of Science Editors:

Muncks JP. Methods for Identifying Cost-efficient Tracking Solutions for Interplanetary Spacecraft. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23702


University of Cincinnati

14. Dadhich, Anang. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 This thesis concentrates on developing an innovative method to generate thrust force for spacecraft in localized geomagnetic fields by various electromagnetic systems. The proposed electromagnetic… (more)

Subjects/Keywords: Aerospace Materials; Electromagnetic Propulsion; Superconductivity; Cryogenics; Spacecraft; Satellite; Spacecraft Propulsion

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APA (6th Edition):

Dadhich, A. (2016). Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799

Chicago Manual of Style (16th Edition):

Dadhich, Anang. “Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.” 2016. Masters Thesis, University of Cincinnati. Accessed June 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799.

MLA Handbook (7th Edition):

Dadhich, Anang. “Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors.” 2016. Web. 20 Jun 2019.

Vancouver:

Dadhich A. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2019 Jun 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799.

Council of Science Editors:

Dadhich A. Electromagnetic Propulsion System for Spacecraft using Geomagnetic Fields and Superconductors. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1461592799

15. Shear, Eric Magnus. Small Spacecraft for Planetary Exploration.

Degree: MSc -MS, Earth & Space Science, 2018, York University

 After an overview of the progress that have been made in small spacecraft for planetary exploration, two planetary mission studies utilizing small spacecraft technologies are… (more)

Subjects/Keywords: Planetology; CubeSats; Spacecraft networks; Small spacecraft; Saturn; Rings; Planetary science

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

APA (6th Edition):

Shear, E. M. (2018). Small Spacecraft for Planetary Exploration. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/34545

Chicago Manual of Style (16th Edition):

Shear, Eric Magnus. “Small Spacecraft for Planetary Exploration.” 2018. Masters Thesis, York University. Accessed June 20, 2019. http://hdl.handle.net/10315/34545.

MLA Handbook (7th Edition):

Shear, Eric Magnus. “Small Spacecraft for Planetary Exploration.” 2018. Web. 20 Jun 2019.

Vancouver:

Shear EM. Small Spacecraft for Planetary Exploration. [Internet] [Masters thesis]. York University; 2018. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/10315/34545.

Council of Science Editors:

Shear EM. Small Spacecraft for Planetary Exploration. [Masters Thesis]. York University; 2018. Available from: http://hdl.handle.net/10315/34545


Virginia Tech

16. Berryman, John Fagan. Analytical and Numerical Analysis of Static Coulomb Formations.

Degree: MS, Aerospace and Ocean Engineering, 2005, Virginia Tech

 For close proximity flying on the order of 10-100 meters, Coulomb thrusting presents a promising alternative to other methods of propulsion. This clean and fuel-efficient… (more)

Subjects/Keywords: Spacecraft Formation; Coulomb Spacecraft

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APA (6th Edition):

Berryman, J. F. (2005). Analytical and Numerical Analysis of Static Coulomb Formations. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36000

Chicago Manual of Style (16th Edition):

Berryman, John Fagan. “Analytical and Numerical Analysis of Static Coulomb Formations.” 2005. Masters Thesis, Virginia Tech. Accessed June 20, 2019. http://hdl.handle.net/10919/36000.

MLA Handbook (7th Edition):

Berryman, John Fagan. “Analytical and Numerical Analysis of Static Coulomb Formations.” 2005. Web. 20 Jun 2019.

Vancouver:

Berryman JF. Analytical and Numerical Analysis of Static Coulomb Formations. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/10919/36000.

Council of Science Editors:

Berryman JF. Analytical and Numerical Analysis of Static Coulomb Formations. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/36000


Indian Institute of Science

17. Indra, A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.

Degree: 2011, Indian Institute of Science

 Presently, most spacecraft are controlled from ground involving activities such as up-linking the schedule of daily operations and monitoring health parameters. These activities lead to… (more)

Subjects/Keywords: Spacecraft Autonomy; Autonomous Spacecraft - Software Architecture; Petri Nets; Petri Net Framework; Autonmous Spacecraft - Multi-Agent Architecture; Petri Net Models; Computer Science

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

APA (6th Edition):

Indra, A. (2011). Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2353

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):

Indra, A. “Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.” 2011. Thesis, Indian Institute of Science. Accessed June 20, 2019. http://hdl.handle.net/2005/2353.

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

MLA Handbook (7th Edition):

Indra, A. “Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.” 2011. Web. 20 Jun 2019.

Vancouver:

Indra A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/2005/2353.

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

Council of Science Editors:

Indra A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. [Thesis]. Indian Institute of Science; 2011. Available from: http://hdl.handle.net/2005/2353

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


Indian Institute of Science

18. Indra, A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.

Degree: 2011, Indian Institute of Science

 Presently, most spacecraft are controlled from ground involving activities such as up-linking the schedule of daily operations and monitoring health parameters. These activities lead to… (more)

Subjects/Keywords: Spacecraft Autonomy; Autonomous Spacecraft - Software Architecture; Petri Nets; Petri Net Framework; Autonmous Spacecraft - Multi-Agent Architecture; Petri Net Models; Computer Science

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

APA (6th Edition):

Indra, A. (2011). Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2353 ; http://etd.ncsi.iisc.ernet.in/abstracts/3026/G24766-Abs.pdf

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):

Indra, A. “Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.” 2011. Thesis, Indian Institute of Science. Accessed June 20, 2019. http://etd.iisc.ernet.in/handle/2005/2353 ; http://etd.ncsi.iisc.ernet.in/abstracts/3026/G24766-Abs.pdf.

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

MLA Handbook (7th Edition):

Indra, A. “Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework.” 2011. Web. 20 Jun 2019.

Vancouver:

Indra A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2019 Jun 20]. Available from: http://etd.iisc.ernet.in/handle/2005/2353 ; http://etd.ncsi.iisc.ernet.in/abstracts/3026/G24766-Abs.pdf.

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

Council of Science Editors:

Indra A. Autonomous Spacecraft Mission Planning And Execution In A Petri Net Framework. [Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ernet.in/handle/2005/2353 ; http://etd.ncsi.iisc.ernet.in/abstracts/3026/G24766-Abs.pdf

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


Lehigh University

19. Zhu, Shiqiao. Analysis of Spacecraft Attitude Control.

Degree: MS, Mechanical Engineering, 2016, Lehigh University

 The thesis studies about repositioning the spacecraft to obtain a moving target problem. We model the spacecraft as a rigid body with axis torque controlling… (more)

Subjects/Keywords: alalysis of spacecraft attitude control; analysis control; attitude; attitude control; attitude of spacecraft; spacecraft control; Engineering; Mechanical Engineering

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

APA (6th Edition):

Zhu, S. (2016). Analysis of Spacecraft Attitude Control. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2915

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):

Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Thesis, Lehigh University. Accessed June 20, 2019. https://preserve.lehigh.edu/etd/2915.

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

MLA Handbook (7th Edition):

Zhu, Shiqiao. “Analysis of Spacecraft Attitude Control.” 2016. Web. 20 Jun 2019.

Vancouver:

Zhu S. Analysis of Spacecraft Attitude Control. [Internet] [Thesis]. Lehigh University; 2016. [cited 2019 Jun 20]. Available from: https://preserve.lehigh.edu/etd/2915.

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

Council of Science Editors:

Zhu S. Analysis of Spacecraft Attitude Control. [Thesis]. Lehigh University; 2016. Available from: https://preserve.lehigh.edu/etd/2915

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


Texas A&M University

20. Hart, Jeremy Jay. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.

Degree: 2009, Texas A&M University

 The Crew Exploration Vehicle (CEV) necessitates higher levels of automation than previous NASA vehicles due to program requirements for automation, including Automated Rendezvous and Docking… (more)

Subjects/Keywords: Automation; Spacecraft; Rendezvous; Decision-making; Fuzzy Logic

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

APA (6th Edition):

Hart, J. J. (2009). Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1220

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):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Thesis, Texas A&M University. Accessed June 20, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1220.

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

MLA Handbook (7th Edition):

Hart, Jeremy Jay. “Methodology for prototyping increased levels of automation for spacecraft rendezvous functions.” 2009. Web. 20 Jun 2019.

Vancouver:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220.

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

Council of Science Editors:

Hart JJ. Methodology for prototyping increased levels of automation for spacecraft rendezvous functions. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1220

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


Texas A&M University

21. Morris, Jeffery C. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.

Degree: 2010, Texas A&M University

 Automated spacecraft docking is a concept of operations with several important potential applications. One application that has received a great deal of attention recently is… (more)

Subjects/Keywords: Spacecraft docking; Vision-based sensors; relative navigation

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APA (6th Edition):

Morris, J. C. (2010). Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820

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):

Morris, Jeffery C. “Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.” 2010. Thesis, Texas A&M University. Accessed June 20, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820.

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

MLA Handbook (7th Edition):

Morris, Jeffery C. “Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor.” 2010. Web. 20 Jun 2019.

Vancouver:

Morris JC. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820.

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

Council of Science Editors:

Morris JC. Automated Spacecraft Docking Using a Vision-Based Relative Navigation Sensor. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2820

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


Cornell University

22. Jones, Laura. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .

Degree: 2012, Cornell University

 Advanced space systems are increasingly reliant on close-proximity operations to achieve complex mission objectives on orbit. These maneuvers - such as docking and rendezvous, formation… (more)

Subjects/Keywords: Flux-pinned interface; spacecraft technology; superconducting physics

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APA (6th Edition):

Jones, L. (2012). The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/31088

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):

Jones, Laura. “The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .” 2012. Thesis, Cornell University. Accessed June 20, 2019. http://hdl.handle.net/1813/31088.

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

MLA Handbook (7th Edition):

Jones, Laura. “The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment .” 2012. Web. 20 Jun 2019.

Vancouver:

Jones L. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . [Internet] [Thesis]. Cornell University; 2012. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1813/31088.

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

Council of Science Editors:

Jones L. The Dynamics And Control Of Flux-Pinned Space Systems: Theory And Experiment . [Thesis]. Cornell University; 2012. Available from: http://hdl.handle.net/1813/31088

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


Georgia Tech

23. Choi, Su Yeon. Automatic mass balancing system for the 5-DOF spacecraft simulator.

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

Spacecraft simulators are widely used to validate spacecraft attitude determination and control techniques. The Autonomous Spacecraft Testing of Robotic Operations in Space (ASTROS) facility at… (more)

Subjects/Keywords: Balancing system; Control; PID; EKF; Spacecraft

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APA (6th Edition):

Choi, S. Y. (2016). Automatic mass balancing system for the 5-DOF spacecraft simulator. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55658

Chicago Manual of Style (16th Edition):

Choi, Su Yeon. “Automatic mass balancing system for the 5-DOF spacecraft simulator.” 2016. Masters Thesis, Georgia Tech. Accessed June 20, 2019. http://hdl.handle.net/1853/55658.

MLA Handbook (7th Edition):

Choi, Su Yeon. “Automatic mass balancing system for the 5-DOF spacecraft simulator.” 2016. Web. 20 Jun 2019.

Vancouver:

Choi SY. Automatic mass balancing system for the 5-DOF spacecraft simulator. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1853/55658.

Council of Science Editors:

Choi SY. Automatic mass balancing system for the 5-DOF spacecraft simulator. [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55658


University of Surrey

24. Farhan, A. H. Dynamic and vibrational analyses of skeletal extraterrestrial structures.

Degree: PhD, 1988, University of Surrey

Subjects/Keywords: 629.47; Manned spacecraft

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APA (6th Edition):

Farhan, A. H. (1988). Dynamic and vibrational analyses of skeletal extraterrestrial structures. (Doctoral Dissertation). University of Surrey. Retrieved from http://epubs.surrey.ac.uk/2164/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.233077

Chicago Manual of Style (16th Edition):

Farhan, A H. “Dynamic and vibrational analyses of skeletal extraterrestrial structures.” 1988. Doctoral Dissertation, University of Surrey. Accessed June 20, 2019. http://epubs.surrey.ac.uk/2164/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.233077.

MLA Handbook (7th Edition):

Farhan, A H. “Dynamic and vibrational analyses of skeletal extraterrestrial structures.” 1988. Web. 20 Jun 2019.

Vancouver:

Farhan AH. Dynamic and vibrational analyses of skeletal extraterrestrial structures. [Internet] [Doctoral dissertation]. University of Surrey; 1988. [cited 2019 Jun 20]. Available from: http://epubs.surrey.ac.uk/2164/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.233077.

Council of Science Editors:

Farhan AH. Dynamic and vibrational analyses of skeletal extraterrestrial structures. [Doctoral Dissertation]. University of Surrey; 1988. Available from: http://epubs.surrey.ac.uk/2164/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.233077


Cleveland State University

25. Jurns, John M. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.

Degree: MSin Mechanical Engineering, Fenn College of Engineering, 2007, Cleveland State University

 Cryogenic fluid systems are fundamental to space flight architecture. Due to the unique properties of cryogenic fluids and the environments in which they operate for… (more)

Subjects/Keywords: Cryogenic; refrigeration; Joule-Thomson; spacecraft; fluid management

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APA (6th Edition):

Jurns, J. M. (2007). Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. (Masters Thesis). Cleveland State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696

Chicago Manual of Style (16th Edition):

Jurns, John M. “Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.” 2007. Masters Thesis, Cleveland State University. Accessed June 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696.

MLA Handbook (7th Edition):

Jurns, John M. “Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions.” 2007. Web. 20 Jun 2019.

Vancouver:

Jurns JM. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. [Internet] [Masters thesis]. Cleveland State University; 2007. [cited 2019 Jun 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696.

Council of Science Editors:

Jurns JM. Flow of Sub-Cooled Cryogens Through a Joule-Thomson Device – Investigation of Metastability Conditions. [Masters Thesis]. Cleveland State University; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=csu1198954696


Penn State University

26. Abaimov, Mikhail D. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.

Degree: MS, Aerospace Engineering, 2015, Penn State University

 CubeSats are small satellites that conform to combinations of a standard 10×10×10 cm form factor. Currently, CubeSats have limited propulsion options because their restrictive size.… (more)

Subjects/Keywords: microwave; electrothermal; thruster; CubeSat; small; spacecraft

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APA (6th Edition):

Abaimov, M. D. (2015). Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26633

Chicago Manual of Style (16th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Masters Thesis, Penn State University. Accessed June 20, 2019. https://etda.libraries.psu.edu/catalog/26633.

MLA Handbook (7th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Web. 20 Jun 2019.

Vancouver:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Internet] [Masters thesis]. Penn State University; 2015. [cited 2019 Jun 20]. Available from: https://etda.libraries.psu.edu/catalog/26633.

Council of Science Editors:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Masters Thesis]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26633


Penn State University

27. Peterson-Burch, Shea Donald Forrest. A Reusable Spacecraft Command and Telemetry Storage Framework.

Degree: MS, Aerospace Engineering, 2009, Penn State University

 The problem of successfully managing the ever increasing quantity of spacecraft commands and telemetry involved in today’s typical spacecraft missions demands building a standardized spacecraft(more)

Subjects/Keywords: spacecraft; commands; telemetry; command and telemetry database

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APA (6th Edition):

Peterson-Burch, S. D. F. (2009). A Reusable Spacecraft Command and Telemetry Storage Framework. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9696

Chicago Manual of Style (16th Edition):

Peterson-Burch, Shea Donald Forrest. “A Reusable Spacecraft Command and Telemetry Storage Framework.” 2009. Masters Thesis, Penn State University. Accessed June 20, 2019. https://etda.libraries.psu.edu/catalog/9696.

MLA Handbook (7th Edition):

Peterson-Burch, Shea Donald Forrest. “A Reusable Spacecraft Command and Telemetry Storage Framework.” 2009. Web. 20 Jun 2019.

Vancouver:

Peterson-Burch SDF. A Reusable Spacecraft Command and Telemetry Storage Framework. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Jun 20]. Available from: https://etda.libraries.psu.edu/catalog/9696.

Council of Science Editors:

Peterson-Burch SDF. A Reusable Spacecraft Command and Telemetry Storage Framework. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9696


Penn State University

28. Hassa, Christopher Louis. Drag Coefficient Estimation using Satellite Attitude and Orbit Data.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 The coefficient of drag for spacecraft in a variety of orbits and solar cycle conditions is generally assumed to be a constant value of 2.2.… (more)

Subjects/Keywords: Swift; coefficient of drag; spacecraft drag coefficient

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APA (6th Edition):

Hassa, C. L. (2013). Drag Coefficient Estimation using Satellite Attitude and Orbit Data. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19949

Chicago Manual of Style (16th Edition):

Hassa, Christopher Louis. “Drag Coefficient Estimation using Satellite Attitude and Orbit Data.” 2013. Masters Thesis, Penn State University. Accessed June 20, 2019. https://etda.libraries.psu.edu/catalog/19949.

MLA Handbook (7th Edition):

Hassa, Christopher Louis. “Drag Coefficient Estimation using Satellite Attitude and Orbit Data.” 2013. Web. 20 Jun 2019.

Vancouver:

Hassa CL. Drag Coefficient Estimation using Satellite Attitude and Orbit Data. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Jun 20]. Available from: https://etda.libraries.psu.edu/catalog/19949.

Council of Science Editors:

Hassa CL. Drag Coefficient Estimation using Satellite Attitude and Orbit Data. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19949


Cornell University

29. Norman, Michael. Integrals Of Motion For Fractionated Space Systems .

Degree: 2011, Cornell University

 As space system architectures begin to rely upon cooperation between multiple spacecraft to perform a single task, the analysis and control of the relative motion… (more)

Subjects/Keywords: Spacecraft; Integrals of Motion; Parameter Estimation

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APA (6th Edition):

Norman, M. (2011). Integrals Of Motion For Fractionated Space Systems . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/30688

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):

Norman, Michael. “Integrals Of Motion For Fractionated Space Systems .” 2011. Thesis, Cornell University. Accessed June 20, 2019. http://hdl.handle.net/1813/30688.

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

MLA Handbook (7th Edition):

Norman, Michael. “Integrals Of Motion For Fractionated Space Systems .” 2011. Web. 20 Jun 2019.

Vancouver:

Norman M. Integrals Of Motion For Fractionated Space Systems . [Internet] [Thesis]. Cornell University; 2011. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1813/30688.

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

Council of Science Editors:

Norman M. Integrals Of Motion For Fractionated Space Systems . [Thesis]. Cornell University; 2011. Available from: http://hdl.handle.net/1813/30688

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


University of Toronto

30. Chari, Navin. Spacecraft Thermal Design Optimization.

Degree: 2009, University of Toronto

Spacecraft thermal design is an inverse problem that requires one to determine the choice of surface properties that yield a desired temperature distribution within a… (more)

Subjects/Keywords: Spacecraft Design; Thermal Optimization; 0756; 0538; 0548

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APA (6th Edition):

Chari, N. (2009). Spacecraft Thermal Design Optimization. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/17501

Chicago Manual of Style (16th Edition):

Chari, Navin. “Spacecraft Thermal Design Optimization.” 2009. Masters Thesis, University of Toronto. Accessed June 20, 2019. http://hdl.handle.net/1807/17501.

MLA Handbook (7th Edition):

Chari, Navin. “Spacecraft Thermal Design Optimization.” 2009. Web. 20 Jun 2019.

Vancouver:

Chari N. Spacecraft Thermal Design Optimization. [Internet] [Masters thesis]. University of Toronto; 2009. [cited 2019 Jun 20]. Available from: http://hdl.handle.net/1807/17501.

Council of Science Editors:

Chari N. Spacecraft Thermal Design Optimization. [Masters Thesis]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/17501

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