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You searched for subject:(CubeSat). Showing records 1 – 30 of 208 total matches.

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Mississippi State University

1. El Brouzi, Ayoub. Orbital study of MSU CubeSat.

Degree: MS, Aerospace Engineering, 2016, Mississippi State University

  The project is an orbital design study of a proposed CubeSat at Mississippi State University. The launch date is not specified. As for the… (more)

Subjects/Keywords: Orbital; CubeSat

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APA (6th Edition):

El Brouzi, A. (2016). Orbital study of MSU CubeSat. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-06292016-125032/ ;

Chicago Manual of Style (16th Edition):

El Brouzi, Ayoub. “Orbital study of MSU CubeSat.” 2016. Masters Thesis, Mississippi State University. Accessed July 19, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-06292016-125032/ ;.

MLA Handbook (7th Edition):

El Brouzi, Ayoub. “Orbital study of MSU CubeSat.” 2016. Web. 19 Jul 2019.

Vancouver:

El Brouzi A. Orbital study of MSU CubeSat. [Internet] [Masters thesis]. Mississippi State University; 2016. [cited 2019 Jul 19]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-06292016-125032/ ;.

Council of Science Editors:

El Brouzi A. Orbital study of MSU CubeSat. [Masters Thesis]. Mississippi State University; 2016. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-06292016-125032/ ;


Texas A&M University

2. Malawey, David Paul. Mechanical Design and Optimization of a Standardized Cubesat.

Degree: MS, Mechanical Engineering, 2016, Texas A&M University

 Cubesats are tiny space exploration vessels with a lower cost than most satellites in history. Rapidly, studies are taking place on this technology to the… (more)

Subjects/Keywords: optimization; cubesat

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APA (6th Edition):

Malawey, D. P. (2016). Mechanical Design and Optimization of a Standardized Cubesat. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/174238

Chicago Manual of Style (16th Edition):

Malawey, David Paul. “Mechanical Design and Optimization of a Standardized Cubesat.” 2016. Masters Thesis, Texas A&M University. Accessed July 19, 2019. http://hdl.handle.net/1969.1/174238.

MLA Handbook (7th Edition):

Malawey, David Paul. “Mechanical Design and Optimization of a Standardized Cubesat.” 2016. Web. 19 Jul 2019.

Vancouver:

Malawey DP. Mechanical Design and Optimization of a Standardized Cubesat. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/1969.1/174238.

Council of Science Editors:

Malawey DP. Mechanical Design and Optimization of a Standardized Cubesat. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/174238


Mississippi State University

3. Zangeneh, Sepehr. Development of a 2U CubeSat for imaging the 2017 solar eclipse.

Degree: MS, Aerospace Engineering, 2018, Mississippi State University

 The entire contiguous United States experienced a solar eclipse on August 21st, 2017 which passed from the Pacific to the Atlantic Coasts. The path of… (more)

Subjects/Keywords: CubeSat; solar eclipse

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APA (6th Edition):

Zangeneh, S. (2018). Development of a 2U CubeSat for imaging the 2017 solar eclipse. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-03202018-080222/ ;

Chicago Manual of Style (16th Edition):

Zangeneh, Sepehr. “Development of a 2U CubeSat for imaging the 2017 solar eclipse.” 2018. Masters Thesis, Mississippi State University. Accessed July 19, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-03202018-080222/ ;.

MLA Handbook (7th Edition):

Zangeneh, Sepehr. “Development of a 2U CubeSat for imaging the 2017 solar eclipse.” 2018. Web. 19 Jul 2019.

Vancouver:

Zangeneh S. Development of a 2U CubeSat for imaging the 2017 solar eclipse. [Internet] [Masters thesis]. Mississippi State University; 2018. [cited 2019 Jul 19]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03202018-080222/ ;.

Council of Science Editors:

Zangeneh S. Development of a 2U CubeSat for imaging the 2017 solar eclipse. [Masters Thesis]. Mississippi State University; 2018. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03202018-080222/ ;


Luleå University of Technology

4. Munteanu, Alexandru Catalin. Nanosat / Cubesat constellation concepts.

Degree: 2009, Luleå University of Technology

This thesis was produced at Cranfield University, with support from EADS Astrium who introduced the base requirements for the study. The subject to be… (more)

Subjects/Keywords: Technology; Cubesat; Teknik

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APA (6th Edition):

Munteanu, A. C. (2009). Nanosat / Cubesat constellation concepts. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47760

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):

Munteanu, Alexandru Catalin. “Nanosat / Cubesat constellation concepts.” 2009. Thesis, Luleå University of Technology. Accessed July 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47760.

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

MLA Handbook (7th Edition):

Munteanu, Alexandru Catalin. “Nanosat / Cubesat constellation concepts.” 2009. Web. 19 Jul 2019.

Vancouver:

Munteanu AC. Nanosat / Cubesat constellation concepts. [Internet] [Thesis]. Luleå University of Technology; 2009. [cited 2019 Jul 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47760.

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

Council of Science Editors:

Munteanu AC. Nanosat / Cubesat constellation concepts. [Thesis]. Luleå University of Technology; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-47760

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


University of Southern California

5. Atchison, Louis Edward, IV. Increased fidelity space weather data collection using a non-linear CubeSat network.

Degree: PhD, Astronautical Engineering, 2009, University of Southern California

 Our understanding of the Low Earth Orbit (LEO) space environment is limited by data collected from in-situ space borne instrumentation. Localized variations in this environment… (more)

Subjects/Keywords: CubeSat; CubeSat network; in-situ space weather data collection; nonlinear CubeSat network; CubeSat space weather

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APA (6th Edition):

Atchison, Louis Edward, I. (2009). Increased fidelity space weather data collection using a non-linear CubeSat network. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/259418/rec/3444

Chicago Manual of Style (16th Edition):

Atchison, Louis Edward, IV. “Increased fidelity space weather data collection using a non-linear CubeSat network.” 2009. Doctoral Dissertation, University of Southern California. Accessed July 19, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/259418/rec/3444.

MLA Handbook (7th Edition):

Atchison, Louis Edward, IV. “Increased fidelity space weather data collection using a non-linear CubeSat network.” 2009. Web. 19 Jul 2019.

Vancouver:

Atchison, Louis Edward I. Increased fidelity space weather data collection using a non-linear CubeSat network. [Internet] [Doctoral dissertation]. University of Southern California; 2009. [cited 2019 Jul 19]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/259418/rec/3444.

Council of Science Editors:

Atchison, Louis Edward I. Increased fidelity space weather data collection using a non-linear CubeSat network. [Doctoral Dissertation]. University of Southern California; 2009. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/259418/rec/3444

6. Pinto Jayawardena, Talini. Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers.

Degree: PhD, 2015, University of Bath

 This research demonstrates the potential of novel technology for space-based remote sensing of the topside ionosphere-plasmasphere, supported by ionospheric imaging, which can augment and enhance… (more)

Subjects/Keywords: 621.384; Plasmapshere, CubeSat, GPS, Tomography

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APA (6th Edition):

Pinto Jayawardena, T. (2015). Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers. (Doctoral Dissertation). University of Bath. Retrieved from https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669039

Chicago Manual of Style (16th Edition):

Pinto Jayawardena, Talini. “Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers.” 2015. Doctoral Dissertation, University of Bath. Accessed July 19, 2019. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669039.

MLA Handbook (7th Edition):

Pinto Jayawardena, Talini. “Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers.” 2015. Web. 19 Jul 2019.

Vancouver:

Pinto Jayawardena T. Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers. [Internet] [Doctoral dissertation]. University of Bath; 2015. [cited 2019 Jul 19]. Available from: https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669039.

Council of Science Editors:

Pinto Jayawardena T. Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers. [Doctoral Dissertation]. University of Bath; 2015. Available from: https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669039


Delft University of Technology

7. Krusharev, I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:.

Degree: 2015, Delft University of Technology

 The format and size specifications of the CubeSat platform require highly miniaturized subsystems, one of the most challenging ones being the propulsion system. Up to… (more)

Subjects/Keywords: propulsion; CubeSat; DelFFi; satellite

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APA (6th Edition):

Krusharev, I. (2015). Micro - Thruster Development: Propulsion System for the DelFFi Mission:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69

Chicago Manual of Style (16th Edition):

Krusharev, I. “Micro - Thruster Development: Propulsion System for the DelFFi Mission:.” 2015. Masters Thesis, Delft University of Technology. Accessed July 19, 2019. http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69.

MLA Handbook (7th Edition):

Krusharev, I. “Micro - Thruster Development: Propulsion System for the DelFFi Mission:.” 2015. Web. 19 Jul 2019.

Vancouver:

Krusharev I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Jul 19]. Available from: http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69.

Council of Science Editors:

Krusharev I. Micro - Thruster Development: Propulsion System for the DelFFi Mission:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69


University of Illinois – Urbana-Champaign

8. Morgan, Jonathan Deming. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.

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

 Spectral radiation is sensitive to many physical chemical aspects of high-enthalpy, non-equilibrium flows affect radiation and heat transfer estimates at low-earth altitudes, which is important… (more)

Subjects/Keywords: hypersonic; nonequilibrium; cubesat; DSMC

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APA (6th Edition):

Morgan, J. D. (2018). Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101076

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):

Morgan, Jonathan Deming. “Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed July 19, 2019. http://hdl.handle.net/2142/101076.

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

MLA Handbook (7th Edition):

Morgan, Jonathan Deming. “Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.” 2018. Web. 19 Jul 2019.

Vancouver:

Morgan JD. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/2142/101076.

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

Council of Science Editors:

Morgan JD. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101076

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


San Jose State University

9. Dinh, Dai. Thermal Modeling of Nanosat.

Degree: MS, Mechanical and Aerospace Engineering, 2012, San Jose State University

  Miniaturization of electronic components enabled small scale satellite projects, such as the CubeSat, to be used for scientific research in space. Recently a team… (more)

Subjects/Keywords: CubeSat; Nanosat; Thermal Modeling

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APA (6th Edition):

Dinh, D. (2012). Thermal Modeling of Nanosat. (Masters Thesis). San Jose State University. Retrieved from https://scholarworks.sjsu.edu/etd_theses/4193

Chicago Manual of Style (16th Edition):

Dinh, Dai. “Thermal Modeling of Nanosat.” 2012. Masters Thesis, San Jose State University. Accessed July 19, 2019. https://scholarworks.sjsu.edu/etd_theses/4193.

MLA Handbook (7th Edition):

Dinh, Dai. “Thermal Modeling of Nanosat.” 2012. Web. 19 Jul 2019.

Vancouver:

Dinh D. Thermal Modeling of Nanosat. [Internet] [Masters thesis]. San Jose State University; 2012. [cited 2019 Jul 19]. Available from: https://scholarworks.sjsu.edu/etd_theses/4193.

Council of Science Editors:

Dinh D. Thermal Modeling of Nanosat. [Masters Thesis]. San Jose State University; 2012. Available from: https://scholarworks.sjsu.edu/etd_theses/4193


Brno University of Technology

10. Pavlík, Arnošt. Napájecí zdroj pro družicové aplikace .

Degree: 2017, Brno University of Technology

 Bakalářské práce spočívá v návrhu a realizaci spínaného zdroje pro použití v satelitech typu Cubesat. V dokumentu jsou popsány teoretické poznatky týkaje se spínaných zdrojů.… (more)

Subjects/Keywords: Spínaný zdroj; měnič; satelit; Cubesat.; Switching power supply; convertor; satellite; Cubesat.

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APA (6th Edition):

Pavlík, A. (2017). Napájecí zdroj pro družicové aplikace . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/68196

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):

Pavlík, Arnošt. “Napájecí zdroj pro družicové aplikace .” 2017. Thesis, Brno University of Technology. Accessed July 19, 2019. http://hdl.handle.net/11012/68196.

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

MLA Handbook (7th Edition):

Pavlík, Arnošt. “Napájecí zdroj pro družicové aplikace .” 2017. Web. 19 Jul 2019.

Vancouver:

Pavlík A. Napájecí zdroj pro družicové aplikace . [Internet] [Thesis]. Brno University of Technology; 2017. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/11012/68196.

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

Council of Science Editors:

Pavlík A. Napájecí zdroj pro družicové aplikace . [Thesis]. Brno University of Technology; 2017. Available from: http://hdl.handle.net/11012/68196

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


Penn State University

11. 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 July 19, 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. 19 Jul 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 Jul 19]. 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


Virginia Tech

12. Fanelli, Lucy Katharine. Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms.

Degree: MS, Electrical and Computer Engineering, 2014, Virginia Tech

 A retarding potential analyzer (RPA) is an instrument that, when mounted on a satellite in low-Earth orbit, makes in-situ measurements of ion density, temperature and… (more)

Subjects/Keywords: retarding potential analyzer; cubesat; instrument electrical design

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APA (6th Edition):

Fanelli, L. K. (2014). Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49297

Chicago Manual of Style (16th Edition):

Fanelli, Lucy Katharine. “Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms.” 2014. Masters Thesis, Virginia Tech. Accessed July 19, 2019. http://hdl.handle.net/10919/49297.

MLA Handbook (7th Edition):

Fanelli, Lucy Katharine. “Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms.” 2014. Web. 19 Jul 2019.

Vancouver:

Fanelli LK. Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/10919/49297.

Council of Science Editors:

Fanelli LK. Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49297


Virginia Tech

13. Venkatramanan, Adithya. Design of control electronics for the Ram Energy Distribution Detector.

Degree: MS, Electrical and Computer Engineering, 2015, Virginia Tech

 The bulk motion of the neutral gas at altitudes between about 200 and 600 km is an important factor in predicting the onset of plasma… (more)

Subjects/Keywords: ram wind sensor; cubesat; instrument electrical design

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APA (6th Edition):

Venkatramanan, A. (2015). Design of control electronics for the Ram Energy Distribution Detector. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/56594

Chicago Manual of Style (16th Edition):

Venkatramanan, Adithya. “Design of control electronics for the Ram Energy Distribution Detector.” 2015. Masters Thesis, Virginia Tech. Accessed July 19, 2019. http://hdl.handle.net/10919/56594.

MLA Handbook (7th Edition):

Venkatramanan, Adithya. “Design of control electronics for the Ram Energy Distribution Detector.” 2015. Web. 19 Jul 2019.

Vancouver:

Venkatramanan A. Design of control electronics for the Ram Energy Distribution Detector. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/10919/56594.

Council of Science Editors:

Venkatramanan A. Design of control electronics for the Ram Energy Distribution Detector. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/56594

14. Rohrer, Todd Edward Bloomquist. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.

Degree: MS, Electrical and Computer Engineering, 2017, Virginia Tech

 Neutral gas pressure measurements in low Earth orbit (LEO) can facilitate the monitoring of atmospheric gravity waves, which can trigger instabilities that severely disrupt radio… (more)

Subjects/Keywords: Space; Spacecraft; CubeSat; Instrumentation; Analog Circuit Design

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APA (6th Edition):

Rohrer, T. E. B. (2017). An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/74916

Chicago Manual of Style (16th Edition):

Rohrer, Todd Edward Bloomquist. “An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.” 2017. Masters Thesis, Virginia Tech. Accessed July 19, 2019. http://hdl.handle.net/10919/74916.

MLA Handbook (7th Edition):

Rohrer, Todd Edward Bloomquist. “An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument.” 2017. Web. 19 Jul 2019.

Vancouver:

Rohrer TEB. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/10919/74916.

Council of Science Editors:

Rohrer TEB. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/74916


Luleå University of Technology

15. Razzaghi, Elyas. Design and Qualification of On-Board Computer for Aalto-1 CubeSat.

Degree: 2012, Luleå University of Technology

In this thesis an electrical model of On-Board Computer (OBC) using commercial-off-the-shelf (COTS) components for the first Finnish small satellite, Aalto-1, is designed and… (more)

Subjects/Keywords: Technology; Aalto-1; CubeSat; OBC; Teknik

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APA (6th Edition):

Razzaghi, E. (2012). Design and Qualification of On-Board Computer for Aalto-1 CubeSat. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49604

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):

Razzaghi, Elyas. “Design and Qualification of On-Board Computer for Aalto-1 CubeSat.” 2012. Thesis, Luleå University of Technology. Accessed July 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49604.

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

MLA Handbook (7th Edition):

Razzaghi, Elyas. “Design and Qualification of On-Board Computer for Aalto-1 CubeSat.” 2012. Web. 19 Jul 2019.

Vancouver:

Razzaghi E. Design and Qualification of On-Board Computer for Aalto-1 CubeSat. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2019 Jul 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49604.

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

Council of Science Editors:

Razzaghi E. Design and Qualification of On-Board Computer for Aalto-1 CubeSat. [Thesis]. Luleå University of Technology; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49604

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

16. Flecht, Tobias. Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite.

Degree: Electrical and Space Engineering, 2016, Luleå University of Technology

In the present paper, which was written in collaboration with the Observatory of Paris, thermal models of two CubeSat missions were created. The first… (more)

Subjects/Keywords: Thermal; CIRCUS; PicSat; NanoSatellite; CubeSat; Thermica

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

APA (6th Edition):

Flecht, T. (2016). Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-59925

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):

Flecht, Tobias. “Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite.” 2016. Thesis, Luleå University of Technology. Accessed July 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-59925.

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

MLA Handbook (7th Edition):

Flecht, Tobias. “Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite.” 2016. Web. 19 Jul 2019.

Vancouver:

Flecht T. Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2019 Jul 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-59925.

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

Council of Science Editors:

Flecht T. Thermal modelling of the PICSAT nanosatellite platform and synergetic prestudies of the CIRCUS nanosatellite. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-59925

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


University of Houston

17. Phadnis, Mandar 1988-. Feedback Control of CubeSat for Attitude and Trajectory Corrections.

Degree: Electrical and Computer Engineering, Department of, 2013, University of Houston

 In order to analyze the performance of Cube Satellites with regards to orbit maintenance and attitude maneuvers, a three unit (3U) CubeSat with a mass… (more)

Subjects/Keywords: CubeSat; Small Satellites; Quaternion; Nonlinear; Spherical Harmonic

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

APA (6th Edition):

Phadnis, M. 1. (2013). Feedback Control of CubeSat for Attitude and Trajectory Corrections. (Thesis). University of Houston. Retrieved from http://hdl.handle.net/10657/1553

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):

Phadnis, Mandar 1988-. “Feedback Control of CubeSat for Attitude and Trajectory Corrections.” 2013. Thesis, University of Houston. Accessed July 19, 2019. http://hdl.handle.net/10657/1553.

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

MLA Handbook (7th Edition):

Phadnis, Mandar 1988-. “Feedback Control of CubeSat for Attitude and Trajectory Corrections.” 2013. Web. 19 Jul 2019.

Vancouver:

Phadnis M1. Feedback Control of CubeSat for Attitude and Trajectory Corrections. [Internet] [Thesis]. University of Houston; 2013. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/10657/1553.

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

Council of Science Editors:

Phadnis M1. Feedback Control of CubeSat for Attitude and Trajectory Corrections. [Thesis]. University of Houston; 2013. Available from: http://hdl.handle.net/10657/1553

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


Vanderbilt University

18. Austin, Rebekah Ann. A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment.

Degree: MS, Electrical Engineering, 2016, Vanderbilt University

 CubeSats have become an attractive platform for university-based spacecraft designs because they are cheaper and quicker to launch than full-scale satellites. One way of keeping… (more)

Subjects/Keywords: COTS; GSN; radiation hardness assurance; CubeSat

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APA (6th Edition):

Austin, R. A. (2016). A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment. (Masters Thesis). Vanderbilt University. Retrieved from http://etd.library.vanderbilt.edu/available/etd-06302016-120807/ ;

Chicago Manual of Style (16th Edition):

Austin, Rebekah Ann. “A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment.” 2016. Masters Thesis, Vanderbilt University. Accessed July 19, 2019. http://etd.library.vanderbilt.edu/available/etd-06302016-120807/ ;.

MLA Handbook (7th Edition):

Austin, Rebekah Ann. “A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment.” 2016. Web. 19 Jul 2019.

Vancouver:

Austin RA. A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment. [Internet] [Masters thesis]. Vanderbilt University; 2016. [cited 2019 Jul 19]. Available from: http://etd.library.vanderbilt.edu/available/etd-06302016-120807/ ;.

Council of Science Editors:

Austin RA. A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment. [Masters Thesis]. Vanderbilt University; 2016. Available from: http://etd.library.vanderbilt.edu/available/etd-06302016-120807/ ;


Purdue University

19. Cofer, Anthony George. FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION.

Degree: PhD, Aeronautics and Astronautics, 2014, Purdue University

 Current small sat propulsion systems require a substantial mass fraction of the vehicle involving tradeoffs between useful payload mass and maneuverability. This is also an… (more)

Subjects/Keywords: cubesat; FEMTA; micropropulsion; microthruster; smallsat; thermal valve

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

APA (6th Edition):

Cofer, A. G. (2014). FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/1106

Chicago Manual of Style (16th Edition):

Cofer, Anthony George. “FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION.” 2014. Doctoral Dissertation, Purdue University. Accessed July 19, 2019. https://docs.lib.purdue.edu/open_access_dissertations/1106.

MLA Handbook (7th Edition):

Cofer, Anthony George. “FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION.” 2014. Web. 19 Jul 2019.

Vancouver:

Cofer AG. FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION. [Internet] [Doctoral dissertation]. Purdue University; 2014. [cited 2019 Jul 19]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/1106.

Council of Science Editors:

Cofer AG. FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION. [Doctoral Dissertation]. Purdue University; 2014. Available from: https://docs.lib.purdue.edu/open_access_dissertations/1106

20. Fear, Andrew John. CubeSat autonomous rendezvous and docking software.

Degree: Aerospace Engineering, 2014, University of Texas – Austin

 An autonomous mission manager is being developed for use on CubeSats to perform proximity operations with other vehicles. The mission manager software is designed to… (more)

Subjects/Keywords: CubeSat; Rendezvous

…List of Figures 1.1 The RACE 3U CubeSat [Photo Credit: JPL]… …increasing mission demands and requirements. For example, previous research into CubeSat control… …Technology Roadmap (TA04 and TA05) [3]. The CubeSat Autonomous Rendezvous and… …The CubeSat Standard A CubeSat is any small satellite that adheres to the CubeSat standard… …composed of cubes where each cube is denoted as 1-unit or 1U. According to the CubeSat standard… 

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APA (6th Edition):

Fear, A. J. (2014). CubeSat autonomous rendezvous and docking software. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28249

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):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Thesis, University of Texas – Austin. Accessed July 19, 2019. http://hdl.handle.net/2152/28249.

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

MLA Handbook (7th Edition):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Web. 19 Jul 2019.

Vancouver:

Fear AJ. CubeSat autonomous rendezvous and docking software. [Internet] [Thesis]. University of Texas – Austin; 2014. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/2152/28249.

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

Council of Science Editors:

Fear AJ. CubeSat autonomous rendezvous and docking software. [Thesis]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/28249

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


Brno University of Technology

21. Horký, Jan. Řídicí jednotka pro CubeSat .

Degree: 2017, Brno University of Technology

 Cílem práce je návrh univerzální řídicí jednotky pro CubeSat založené na obvodu FPGA. Taková jednotka doposud nebyla komerčně dostupná a navržená jednotka má tak dobrý… (more)

Subjects/Keywords: Vesmír; CubeSat; Řídicí jednotka; Radiace; FPGA; Space; CubeSat; Control Unit; Radiation; FPGA

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APA (6th Edition):

Horký, J. (2017). Řídicí jednotka pro CubeSat . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/66006

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):

Horký, Jan. “Řídicí jednotka pro CubeSat .” 2017. Thesis, Brno University of Technology. Accessed July 19, 2019. http://hdl.handle.net/11012/66006.

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

MLA Handbook (7th Edition):

Horký, Jan. “Řídicí jednotka pro CubeSat .” 2017. Web. 19 Jul 2019.

Vancouver:

Horký J. Řídicí jednotka pro CubeSat . [Internet] [Thesis]. Brno University of Technology; 2017. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/11012/66006.

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

Council of Science Editors:

Horký J. Řídicí jednotka pro CubeSat . [Thesis]. Brno University of Technology; 2017. Available from: http://hdl.handle.net/11012/66006

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


KTH

22. Jéger, Csaba. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.

Degree: Space and Plasma Physics, 2017, KTH

SEAM (Small Explorer for Advanced Missions) is a 3U CubeSat developedat KTH Royal Institute of Technology which will provide highqualityDC and AC magnetic field… (more)

Subjects/Keywords: cubesat; magnetic dipole estimation; attitude dynamics; cubesat; magnetisk dipol uppskattning; attityddynamik; Electrical Engineering, Electronic Engineering, Information Engineering; Elektroteknik och elektronik

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

APA (6th Edition):

Jéger, C. (2017). Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985

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):

Jéger, Csaba. “Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.” 2017. Thesis, KTH. Accessed July 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985.

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

MLA Handbook (7th Edition):

Jéger, Csaba. “Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission.” 2017. Web. 19 Jul 2019.

Vancouver:

Jéger C. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. [Internet] [Thesis]. KTH; 2017. [cited 2019 Jul 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985.

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

Council of Science Editors:

Jéger C. Determination and compensation of magnetic dipole moment inapplication for a scientific nanosatellite mission. [Thesis]. KTH; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-212985

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

23. Secondo, Raffaello. Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO.

Degree: Docteur es, Électronique, 2017, Montpellier

Les champs radiatifs dans le complexe d’accélérateurs du CERN sont caractérisés par des particules mixtes avec un large spectre d’énergie. Le système de surveillance des… (more)

Subjects/Keywords: Surveillance niveaux de radiation; Qualification Composants Electroniques; Dosimetrie; CubeSat; Environnement Radiatif; Radiation Monitoring; Radiation Qualification; Dosimetry; CubeSat; Radiation Environment

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APA (6th Edition):

Secondo, R. (2017). Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO. (Doctoral Dissertation). Montpellier. Retrieved from http://www.theses.fr/2017MONTS063

Chicago Manual of Style (16th Edition):

Secondo, Raffaello. “Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO.” 2017. Doctoral Dissertation, Montpellier. Accessed July 19, 2019. http://www.theses.fr/2017MONTS063.

MLA Handbook (7th Edition):

Secondo, Raffaello. “Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO.” 2017. Web. 19 Jul 2019.

Vancouver:

Secondo R. Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO. [Internet] [Doctoral dissertation]. Montpellier; 2017. [cited 2019 Jul 19]. Available from: http://www.theses.fr/2017MONTS063.

Council of Science Editors:

Secondo R. Upgrades of the RadMON V6 and its Integration on a Nanosatellite for theAnalysis and the Comparative Study of the CHARM and Low Earth Orbit Environments : Améliorations du RadMON V6 et son intégration dans un nanosatellite pour l’analyse et l’étude comparative des environnements CHARM et LEO. [Doctoral Dissertation]. Montpellier; 2017. Available from: http://www.theses.fr/2017MONTS063


Georgia Tech

24. 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 July 19, 2019. http://hdl.handle.net/1853/55671.

MLA Handbook (7th Edition):

Francis, Parker. “Development of the evolved common hardware bus (TECHBus).” 2016. Web. 19 Jul 2019.

Vancouver:

Francis P. Development of the evolved common hardware bus (TECHBus). [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Jul 19]. 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

25. Nelson, Heather. Low-earth-orbit Target Design for.

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

 In an era in which the orbital space around Earth becomes increasingly crowded with debris, Space Situational Awareness is becoming more and more critical. As… (more)

Subjects/Keywords: Calibration; Falcon Telescope Network; CubeSat; Space Situational Awareness.

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APA (6th Edition):

Nelson, H. (2014). Low-earth-orbit Target Design for. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23465

Chicago Manual of Style (16th Edition):

Nelson, Heather. “Low-earth-orbit Target Design for.” 2014. Masters Thesis, Penn State University. Accessed July 19, 2019. https://etda.libraries.psu.edu/catalog/23465.

MLA Handbook (7th Edition):

Nelson, Heather. “Low-earth-orbit Target Design for.” 2014. Web. 19 Jul 2019.

Vancouver:

Nelson H. Low-earth-orbit Target Design for. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Jul 19]. Available from: https://etda.libraries.psu.edu/catalog/23465.

Council of Science Editors:

Nelson H. Low-earth-orbit Target Design for. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23465


University of California – Santa Cruz

26. Chesi, Simone. ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES.

Degree: Applied Mathematics and Statistics, 2015, University of California – Santa Cruz

 Since the development of the CubeSat standard, the number of nanosatellites developed by universities, federal agencies and commercial companies has greatly increased as well as… (more)

Subjects/Keywords: Aerospace engineering; Robotics; Engineering; autonomous; cubesat; GNC; nanosatellite; nonlinear control; spacecraft

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APA (6th Edition):

Chesi, S. (2015). ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES. (Thesis). University of California – Santa Cruz. Retrieved from http://www.escholarship.org/uc/item/61r1d1sm

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):

Chesi, Simone. “ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES.” 2015. Thesis, University of California – Santa Cruz. Accessed July 19, 2019. http://www.escholarship.org/uc/item/61r1d1sm.

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

MLA Handbook (7th Edition):

Chesi, Simone. “ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES.” 2015. Web. 19 Jul 2019.

Vancouver:

Chesi S. ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES. [Internet] [Thesis]. University of California – Santa Cruz; 2015. [cited 2019 Jul 19]. Available from: http://www.escholarship.org/uc/item/61r1d1sm.

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

Council of Science Editors:

Chesi S. ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES. [Thesis]. University of California – Santa Cruz; 2015. Available from: http://www.escholarship.org/uc/item/61r1d1sm

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


Cape Peninsula University of Technology

27. Maqina, Sinamandla Mvuyisi. X-band antenna design for nano-satellite applications .

Degree: 2018, Cape Peninsula University of Technology

 This research report discusses feasible designs of conformal antennas that provide a proof of concept for the French South African Institute of Technology’s future needs.… (more)

Subjects/Keywords: Antennas (Electronics); Nanosatellites; CubeSat; Microstrip antennas  – Design and construction

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APA (6th Edition):

Maqina, S. M. (2018). X-band antenna design for nano-satellite applications . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/2703

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):

Maqina, Sinamandla Mvuyisi. “X-band antenna design for nano-satellite applications .” 2018. Thesis, Cape Peninsula University of Technology. Accessed July 19, 2019. http://etd.cput.ac.za/handle/20.500.11838/2703.

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

MLA Handbook (7th Edition):

Maqina, Sinamandla Mvuyisi. “X-band antenna design for nano-satellite applications .” 2018. Web. 19 Jul 2019.

Vancouver:

Maqina SM. X-band antenna design for nano-satellite applications . [Internet] [Thesis]. Cape Peninsula University of Technology; 2018. [cited 2019 Jul 19]. Available from: http://etd.cput.ac.za/handle/20.500.11838/2703.

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

Council of Science Editors:

Maqina SM. X-band antenna design for nano-satellite applications . [Thesis]. Cape Peninsula University of Technology; 2018. Available from: http://etd.cput.ac.za/handle/20.500.11838/2703

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


Delft University of Technology

28. Go, S.Y. Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:.

Degree: 2009, Delft University of Technology

 Design of the different elements in the Structural Subsystem of Delfi-n3Xt. This is done by implementation of the lessons learned and solutions to problems encountered… (more)

Subjects/Keywords: Delfi-n3Xt; Structural Subsystem; Arrangement Subsystems and Payload; CubeSat

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APA (6th Edition):

Go, S. Y. (2009). Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dfb12789-54a2-4d11-ba44-82233c0c16c3

Chicago Manual of Style (16th Edition):

Go, S Y. “Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:.” 2009. Masters Thesis, Delft University of Technology. Accessed July 19, 2019. http://resolver.tudelft.nl/uuid:dfb12789-54a2-4d11-ba44-82233c0c16c3.

MLA Handbook (7th Edition):

Go, S Y. “Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:.” 2009. Web. 19 Jul 2019.

Vancouver:

Go SY. Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:. [Internet] [Masters thesis]. Delft University of Technology; 2009. [cited 2019 Jul 19]. Available from: http://resolver.tudelft.nl/uuid:dfb12789-54a2-4d11-ba44-82233c0c16c3.

Council of Science Editors:

Go SY. Mechanical Design and Arrangement of nanosatellite Delfi-n3Xt:. [Masters Thesis]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:dfb12789-54a2-4d11-ba44-82233c0c16c3

29. Pinto Alejo , Brigitte Stefany. DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT .

Degree: 2014, Universidad de los Andes

 El presente documento pretende mostrar el proceso realizado para el diseño de un prototipo de sistema micropropulsor orientado al desorbitaje de satélites CubeSat. Inicialmente se… (more)

Subjects/Keywords: micropropulsor; CubeSat; nanosatélite; desorbitaje

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

APA (6th Edition):

Pinto Alejo , B. S. (2014). DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT . (Thesis). Universidad de los Andes. Retrieved from http://documentodegrado.uniandes.edu.co/documentos/200912652_fecha_2014_07_31_hora_18_03_42_parte_1.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):

Pinto Alejo , Brigitte Stefany. “DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT .” 2014. Thesis, Universidad de los Andes. Accessed July 19, 2019. http://documentodegrado.uniandes.edu.co/documentos/200912652_fecha_2014_07_31_hora_18_03_42_parte_1.pdf.

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

MLA Handbook (7th Edition):

Pinto Alejo , Brigitte Stefany. “DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT .” 2014. Web. 19 Jul 2019.

Vancouver:

Pinto Alejo BS. DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT . [Internet] [Thesis]. Universidad de los Andes; 2014. [cited 2019 Jul 19]. Available from: http://documentodegrado.uniandes.edu.co/documentos/200912652_fecha_2014_07_31_hora_18_03_42_parte_1.pdf.

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

Council of Science Editors:

Pinto Alejo BS. DISEÑO DE UN SISTEMA MICROPROPULSOR PARA EL DESORBITAJE DE SATÉLITES CUBESAT . [Thesis]. Universidad de los Andes; 2014. Available from: http://documentodegrado.uniandes.edu.co/documentos/200912652_fecha_2014_07_31_hora_18_03_42_parte_1.pdf

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


University of Washington

30. Kelly, Charles. Magnetoshell Aerocapture: Advances Toward Concept Feasibility.

Degree: 2018, University of Washington

 Magnetoshell Aerocapture (MAC) is a novel technology that proposes to use drag on a dipole plasma in planetary atmospheres as an orbit insertion technique. It… (more)

Subjects/Keywords: Aerocapture; CubeSat; Magnetoshell; Aerospace engineering; Plasma physics; Aeronautics and astronautics

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

APA (6th Edition):

Kelly, C. (2018). Magnetoshell Aerocapture: Advances Toward Concept Feasibility. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/42172

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):

Kelly, Charles. “Magnetoshell Aerocapture: Advances Toward Concept Feasibility.” 2018. Thesis, University of Washington. Accessed July 19, 2019. http://hdl.handle.net/1773/42172.

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

MLA Handbook (7th Edition):

Kelly, Charles. “Magnetoshell Aerocapture: Advances Toward Concept Feasibility.” 2018. Web. 19 Jul 2019.

Vancouver:

Kelly C. Magnetoshell Aerocapture: Advances Toward Concept Feasibility. [Internet] [Thesis]. University of Washington; 2018. [cited 2019 Jul 19]. Available from: http://hdl.handle.net/1773/42172.

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

Council of Science Editors:

Kelly C. Magnetoshell Aerocapture: Advances Toward Concept Feasibility. [Thesis]. University of Washington; 2018. Available from: http://hdl.handle.net/1773/42172

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

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