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You searched for subject:(cubesat). Showing records 1 – 30 of 256 total matches.

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Texas A&M University

1. 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 September 26, 2020. http://hdl.handle.net/1969.1/174238.

MLA Handbook (7th Edition):

Malawey, David Paul. “Mechanical Design and Optimization of a Standardized Cubesat.” 2016. Web. 26 Sep 2020.

Vancouver:

Malawey DP. Mechanical Design and Optimization of a Standardized Cubesat. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2020 Sep 26]. 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

2. 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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

El Brouzi A. Orbital study of MSU CubeSat. [Internet] [Masters thesis]. Mississippi State University; 2016. [cited 2020 Sep 26]. 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/ ;


Penn State University

3. Garzon, Maria M. DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT .

Degree: 2012, Penn State University

 Proper spacecraft thermal design ensures spacecraft reliability despite the variations in its environment that it will encounter, such as heat inputs from the Sun and… (more)

Subjects/Keywords: CubeSat; OSIRIS-3U; Thermal Design

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APA (6th Edition):

Garzon, M. M. (2012). DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15404

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):

Garzon, Maria M. “DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT .” 2012. Thesis, Penn State University. Accessed September 26, 2020. https://submit-etda.libraries.psu.edu/catalog/15404.

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

MLA Handbook (7th Edition):

Garzon, Maria M. “DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT .” 2012. Web. 26 Sep 2020.

Vancouver:

Garzon MM. DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT . [Internet] [Thesis]. Penn State University; 2012. [cited 2020 Sep 26]. Available from: https://submit-etda.libraries.psu.edu/catalog/15404.

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

Council of Science Editors:

Garzon MM. DEVELOPMENT AND ANALYSIS OF THE THERMAL DESIGN FOR THE OSIRIS-3U CUBESAT . [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/15404

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

4. 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://researchportal.bath.ac.uk/en/studentthesis/topside-ionosphereplasmasphere-tomography-using-spaceborne-dual-frequency-gps-receivers(ceab43d0-c698-483b-aeee-599585845f02).html ; 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 September 26, 2020. https://researchportal.bath.ac.uk/en/studentthesis/topside-ionosphereplasmasphere-tomography-using-spaceborne-dual-frequency-gps-receivers(ceab43d0-c698-483b-aeee-599585845f02).html ; 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. 26 Sep 2020.

Vancouver:

Pinto Jayawardena T. Topside ionosphere/plasmasphere tomography using space-borne dual frequency GPS receivers. [Internet] [Doctoral dissertation]. University of Bath; 2015. [cited 2020 Sep 26]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/topside-ionosphereplasmasphere-tomography-using-spaceborne-dual-frequency-gps-receivers(ceab43d0-c698-483b-aeee-599585845f02).html ; 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://researchportal.bath.ac.uk/en/studentthesis/topside-ionosphereplasmasphere-tomography-using-spaceborne-dual-frequency-gps-receivers(ceab43d0-c698-483b-aeee-599585845f02).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669039


San Jose State University

5. 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://doi.org/10.31979/etd.cx59-auuj ; 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 September 26, 2020. https://doi.org/10.31979/etd.cx59-auuj ; https://scholarworks.sjsu.edu/etd_theses/4193.

MLA Handbook (7th Edition):

Dinh, Dai. “Thermal Modeling of Nanosat.” 2012. Web. 26 Sep 2020.

Vancouver:

Dinh D. Thermal Modeling of Nanosat. [Internet] [Masters thesis]. San Jose State University; 2012. [cited 2020 Sep 26]. Available from: https://doi.org/10.31979/etd.cx59-auuj ; 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://doi.org/10.31979/etd.cx59-auuj ; https://scholarworks.sjsu.edu/etd_theses/4193


Rochester Institute of Technology

6. Loewenthal, Jared A. A 3U Cubesat Platform for Plant Growth Experiments.

Degree: MS, Electrical Engineering, 2019, Rochester Institute of Technology

  This thesis work presents the design, manufacturing, and ground testing of a 3U Cubesat platform intended for plant growth experiments. The structure is comprised… (more)

Subjects/Keywords: Cubesat; Microbiome; Plant growth chambers

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APA (6th Edition):

Loewenthal, J. A. (2019). A 3U Cubesat Platform for Plant Growth Experiments. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/10290

Chicago Manual of Style (16th Edition):

Loewenthal, Jared A. “A 3U Cubesat Platform for Plant Growth Experiments.” 2019. Masters Thesis, Rochester Institute of Technology. Accessed September 26, 2020. https://scholarworks.rit.edu/theses/10290.

MLA Handbook (7th Edition):

Loewenthal, Jared A. “A 3U Cubesat Platform for Plant Growth Experiments.” 2019. Web. 26 Sep 2020.

Vancouver:

Loewenthal JA. A 3U Cubesat Platform for Plant Growth Experiments. [Internet] [Masters thesis]. Rochester Institute of Technology; 2019. [cited 2020 Sep 26]. Available from: https://scholarworks.rit.edu/theses/10290.

Council of Science Editors:

Loewenthal JA. A 3U Cubesat Platform for Plant Growth Experiments. [Masters Thesis]. Rochester Institute of Technology; 2019. Available from: https://scholarworks.rit.edu/theses/10290


Delft University of Technology

7. Krusharev, I. (author). 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 (author). “Micro - Thruster Development: Propulsion System for the DelFFi Mission.” 2015. Masters Thesis, Delft University of Technology. Accessed September 26, 2020. http://resolver.tudelft.nl/uuid:e60e68fe-d1f6-458b-8a5a-d5036e32fb69.

MLA Handbook (7th Edition):

Krusharev, I (author). “Micro - Thruster Development: Propulsion System for the DelFFi Mission.” 2015. Web. 26 Sep 2020.

Vancouver:

Krusharev I(. Micro - Thruster Development: Propulsion System for the DelFFi Mission. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 26]. 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


Delft University of Technology

8. Brouwer, H.S.B. (author). Performance Characterization of Water Heat Pipes and their Application in CubeSats.

Degree: 2016, Delft University of Technology

The CubeSat platform has long since its introduction surpassed its original intend of being an educational and technology demonstration platform only. The recognition and acknowledgement… (more)

Subjects/Keywords: heat pipes; CubeSat; thermal control

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APA (6th Edition):

Brouwer, H. S. B. (. (2016). Performance Characterization of Water Heat Pipes and their Application in CubeSats. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:219151e3-aac4-4cc7-8fb4-535e525d0297

Chicago Manual of Style (16th Edition):

Brouwer, H S B (author). “Performance Characterization of Water Heat Pipes and their Application in CubeSats.” 2016. Masters Thesis, Delft University of Technology. Accessed September 26, 2020. http://resolver.tudelft.nl/uuid:219151e3-aac4-4cc7-8fb4-535e525d0297.

MLA Handbook (7th Edition):

Brouwer, H S B (author). “Performance Characterization of Water Heat Pipes and their Application in CubeSats.” 2016. Web. 26 Sep 2020.

Vancouver:

Brouwer HSB(. Performance Characterization of Water Heat Pipes and their Application in CubeSats. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Sep 26]. Available from: http://resolver.tudelft.nl/uuid:219151e3-aac4-4cc7-8fb4-535e525d0297.

Council of Science Editors:

Brouwer HSB(. Performance Characterization of Water Heat Pipes and their Application in CubeSats. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:219151e3-aac4-4cc7-8fb4-535e525d0297


University of Minnesota

9. Kukowski, Timothy. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.

Degree: MS, Aerospace Engineering and Mechanics, 2020, University of Minnesota

 SOCRATES and IMPRESS are two cubesats designed and built by the University of Minnesota's Small Satellite Team. These satellites have similar build and function by… (more)

Subjects/Keywords: attitude; control; cubesat; magnetic; magnetorquers

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APA (6th Edition):

Kukowski, T. (2020). Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/213061

Chicago Manual of Style (16th Edition):

Kukowski, Timothy. “Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.” 2020. Masters Thesis, University of Minnesota. Accessed September 26, 2020. http://hdl.handle.net/11299/213061.

MLA Handbook (7th Edition):

Kukowski, Timothy. “Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite.” 2020. Web. 26 Sep 2020.

Vancouver:

Kukowski T. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. [Internet] [Masters thesis]. University of Minnesota; 2020. [cited 2020 Sep 26]. Available from: http://hdl.handle.net/11299/213061.

Council of Science Editors:

Kukowski T. Magnetic Attitude Control Development and Simulation for a 3U Cube Satellite. [Masters Thesis]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/213061


University of Illinois – Urbana-Champaign

10. 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 September 26, 2020. 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. 26 Sep 2020.

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 2020 Sep 26]. 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


University of Florida

11. Omar, Sanny R. A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2019, University of Florida

 The ability to re-enter the atmosphere at a desired location is important for spacecraft containing components that may survive re-entry. This work discusses the use… (more)

Subjects/Keywords: control  – cubesat  – drag  – hardware  – reentry

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APA (6th Edition):

Omar, S. R. (2019). A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0055992

Chicago Manual of Style (16th Edition):

Omar, Sanny R. “A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag.” 2019. Doctoral Dissertation, University of Florida. Accessed September 26, 2020. https://ufdc.ufl.edu/UFE0055992.

MLA Handbook (7th Edition):

Omar, Sanny R. “A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag.” 2019. Web. 26 Sep 2020.

Vancouver:

Omar SR. A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag. [Internet] [Doctoral dissertation]. University of Florida; 2019. [cited 2020 Sep 26]. Available from: https://ufdc.ufl.edu/UFE0055992.

Council of Science Editors:

Omar SR. A Drag Device and Control Algorithm for Spacecraft Attitude Stabilization and De-Orbit Point Targeting Using Aerodynamic Drag. [Doctoral Dissertation]. University of Florida; 2019. Available from: https://ufdc.ufl.edu/UFE0055992


University of Florida

12. Serra, Paul Charly. Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2018, University of Florida

 Thanks to the continuous improvement in lasers, high quality and powerful pulsed light sources are now available and can be used to exchange time and… (more)

Subjects/Keywords: clock  – communication  – cubesat  – laser  – time

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APA (6th Edition):

Serra, P. C. (2018). Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0052212

Chicago Manual of Style (16th Edition):

Serra, Paul Charly. “Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication.” 2018. Doctoral Dissertation, University of Florida. Accessed September 26, 2020. https://ufdc.ufl.edu/UFE0052212.

MLA Handbook (7th Edition):

Serra, Paul Charly. “Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication.” 2018. Web. 26 Sep 2020.

Vancouver:

Serra PC. Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication. [Internet] [Doctoral dissertation]. University of Florida; 2018. [cited 2020 Sep 26]. Available from: https://ufdc.ufl.edu/UFE0052212.

Council of Science Editors:

Serra PC. Integrated, Low-Power Sub-Nanosecond Timing Systems For Space Navigation And Communication. [Doctoral Dissertation]. University of Florida; 2018. Available from: https://ufdc.ufl.edu/UFE0052212


Brno University of Technology

13. Pavlík, Arnošt. Napájecí zdroj pro družicové aplikace: Satellite power supply.

Degree: 2019, Brno University of Technology

 The bachelor thesis consists of the design and realization switched source for use in satellites of Cubesat type. The paper describes the theoretical knowledge of… (more)

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

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APA (6th Edition):

Pavlík, A. (2019). Napájecí zdroj pro družicové aplikace: Satellite power supply. (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: Satellite power supply.” 2019. Thesis, Brno University of Technology. Accessed September 26, 2020. 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: Satellite power supply.” 2019. Web. 26 Sep 2020.

Vancouver:

Pavlík A. Napájecí zdroj pro družicové aplikace: Satellite power supply. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Sep 26]. 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: Satellite power supply. [Thesis]. Brno University of Technology; 2019. 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


Vanderbilt University

14. 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. (Thesis). Vanderbilt University. Retrieved from http://hdl.handle.net/1803/12763

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):

Austin, Rebekah Ann. “A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment.” 2016. Thesis, Vanderbilt University. Accessed September 26, 2020. http://hdl.handle.net/1803/12763.

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

MLA Handbook (7th Edition):

Austin, Rebekah Ann. “A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment.” 2016. Web. 26 Sep 2020.

Vancouver:

Austin RA. A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment. [Internet] [Thesis]. Vanderbilt University; 2016. [cited 2020 Sep 26]. Available from: http://hdl.handle.net/1803/12763.

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

Council of Science Editors:

Austin RA. A Radiation-Reliability Assurance Case using Goal Structuring Notation for a CubeSat Experiment. [Thesis]. Vanderbilt University; 2016. Available from: http://hdl.handle.net/1803/12763

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


Penn State University

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

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

APA (6th Edition):

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

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):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Thesis, Penn State University. Accessed September 26, 2020. https://submit-etda.libraries.psu.edu/catalog/26633.

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

MLA Handbook (7th Edition):

Abaimov, Mikhail D. “Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft.” 2015. Web. 26 Sep 2020.

Vancouver:

Abaimov MD. Preliminary Testing of a 17.8-GHz Microwave Electrothermal Thruster for Small Spacecraft. [Internet] [Thesis]. Penn State University; 2015. [cited 2020 Sep 26]. Available from: https://submit-etda.libraries.psu.edu/catalog/26633.

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

Council of Science Editors:

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

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


Virginia Tech

16. 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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

Fanelli LK. Electronics for a Versatile and Robust Retarding Potential Analyzer for Nano-Satellite Platforms. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 26]. 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

17. 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 September 26, 2020. http://hdl.handle.net/10919/56594.

MLA Handbook (7th Edition):

Venkatramanan, Adithya. “Design of control electronics for the Ram Energy Distribution Detector.” 2015. Web. 26 Sep 2020.

Vancouver:

Venkatramanan A. Design of control electronics for the Ram Energy Distribution Detector. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Sep 26]. 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

18. 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

Page 1 Page 2

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

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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

Rohrer TEB. An Electrometer Design and Characterization for a CubeSat Neutral Pressure Instrument. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Sep 26]. 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


Delft University of Technology

19. Paolini, Giovanni (author). FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing.

Degree: 2017, Delft University of Technology

CONTEXT. Spectropolarimetry is proposed as a relatively new option in the field of remote sensing for the characterization of aerosol particles and the investigation of… (more)

Subjects/Keywords: FlySPEX; Spectropolarimetry; Earth Observation; CubeSat; Calibration

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APA (6th Edition):

Paolini, G. (. (2017). FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e4520dd9-0af1-4ee7-b60d-e933d915217e

Chicago Manual of Style (16th Edition):

Paolini, Giovanni (author). “FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing.” 2017. Masters Thesis, Delft University of Technology. Accessed September 26, 2020. http://resolver.tudelft.nl/uuid:e4520dd9-0af1-4ee7-b60d-e933d915217e.

MLA Handbook (7th Edition):

Paolini, Giovanni (author). “FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing.” 2017. Web. 26 Sep 2020.

Vancouver:

Paolini G(. FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Sep 26]. Available from: http://resolver.tudelft.nl/uuid:e4520dd9-0af1-4ee7-b60d-e933d915217e.

Council of Science Editors:

Paolini G(. FlySPEX: Channeled Spectropolarimeter for Atmosphere Remote Sensing. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:e4520dd9-0af1-4ee7-b60d-e933d915217e


Purdue University

20. 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 (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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

Cofer AG. FILM EVAPORATION MEMS THRUSTER ARRAY FOR MICROPROPULSION. [Internet] [Doctoral dissertation]. Purdue University; 2014. [cited 2020 Sep 26]. 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


University of Sydney

21. Maj, Ronald. Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere .

Degree: 2018, University of Sydney

 The practicality of detecting thermal Langmuir waves, charged particle impacts (i.e. ``shot noise”) and impacts from dust particles on a CubeSat in the Earth’s ionosphere… (more)

Subjects/Keywords: CubeSat; Ionosphere; Antenna; Shot-noise; QTN; Monopole

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APA (6th Edition):

Maj, R. (2018). Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/20700

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):

Maj, Ronald. “Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere .” 2018. Thesis, University of Sydney. Accessed September 26, 2020. http://hdl.handle.net/2123/20700.

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

MLA Handbook (7th Edition):

Maj, Ronald. “Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere .” 2018. Web. 26 Sep 2020.

Vancouver:

Maj R. Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere . [Internet] [Thesis]. University of Sydney; 2018. [cited 2020 Sep 26]. Available from: http://hdl.handle.net/2123/20700.

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

Council of Science Editors:

Maj R. Voltage Power Spectroscopy on a CubeSat in Earth's Ionosphere . [Thesis]. University of Sydney; 2018. Available from: http://hdl.handle.net/2123/20700

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

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

Degree: MSin Engineering, 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. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28249

Chicago Manual of Style (16th Edition):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Masters Thesis, University of Texas – Austin. Accessed September 26, 2020. http://hdl.handle.net/2152/28249.

MLA Handbook (7th Edition):

Fear, Andrew John. “CubeSat autonomous rendezvous and docking software.” 2014. Web. 26 Sep 2020.

Vancouver:

Fear AJ. CubeSat autonomous rendezvous and docking software. [Internet] [Masters thesis]. University of Texas – Austin; 2014. [cited 2020 Sep 26]. Available from: http://hdl.handle.net/2152/28249.

Council of Science Editors:

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


University of Houston

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

Degree: MSin Electrical Engineering, Electrical Engineering, 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 harmonics

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Phadnis, Mandar 1988-. “Feedback Control of CubeSat for Attitude and Trajectory Corrections.” 2013. Masters Thesis, University of Houston. Accessed September 26, 2020. http://hdl.handle.net/10657/1553.

MLA Handbook (7th Edition):

Phadnis, Mandar 1988-. “Feedback Control of CubeSat for Attitude and Trajectory Corrections.” 2013. Web. 26 Sep 2020.

Vancouver:

Phadnis M1. Feedback Control of CubeSat for Attitude and Trajectory Corrections. [Internet] [Masters thesis]. University of Houston; 2013. [cited 2020 Sep 26]. Available from: http://hdl.handle.net/10657/1553.

Council of Science Editors:

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


Luleå University of Technology

24. 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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

Razzaghi E. Design and Qualification of On-Board Computer for Aalto-1 CubeSat. [Internet] [Thesis]. Luleå University of Technology; 2012. [cited 2020 Sep 26]. 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


Luleå University of Technology

25. 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 September 26, 2020. 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. 26 Sep 2020.

Vancouver:

Munteanu AC. Nanosat / Cubesat constellation concepts. [Internet] [Thesis]. Luleå University of Technology; 2009. [cited 2020 Sep 26]. 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


Delft University of Technology

26. Gelmi, Samuele (author). Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology.

Degree: 2019, Delft University of Technology

This Thesis presents the design and implementation of a preliminary Fault Detection Isolation and Recovery (FDIR) architecture for LUMIO, a CubeSat mission to the Moon.… (more)

Subjects/Keywords: Fault Detection; Fault Recovery; CubeSat; FMECA

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APA (6th Edition):

Gelmi, S. (. (2019). Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7fd12ea7-b85e-4140-942e-0b9d52d4fa13

Chicago Manual of Style (16th Edition):

Gelmi, Samuele (author). “Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology.” 2019. Masters Thesis, Delft University of Technology. Accessed September 26, 2020. http://resolver.tudelft.nl/uuid:7fd12ea7-b85e-4140-942e-0b9d52d4fa13.

MLA Handbook (7th Edition):

Gelmi, Samuele (author). “Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology.” 2019. Web. 26 Sep 2020.

Vancouver:

Gelmi S(. Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 26]. Available from: http://resolver.tudelft.nl/uuid:7fd12ea7-b85e-4140-942e-0b9d52d4fa13.

Council of Science Editors:

Gelmi S(. Fault Detection Isolation and Recovery for LUMIO mission: Algorithm and Methodology. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:7fd12ea7-b85e-4140-942e-0b9d52d4fa13

27. Martinez, Nicolas. Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere.

Degree: MS, 2015, Worcester Polytechnic Institute

 "Orbital flight of CubeSats in extremely Low Earth Orbit, defined here as an altitude between 150 – 250 km, has the potential to enable a… (more)

Subjects/Keywords: GPS; thermosphere; LEO; CubeSat; electrospray; energy; orbital

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APA (6th Edition):

Martinez, N. (2015). Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere. (Thesis). Worcester Polytechnic Institute. Retrieved from etd-072915-163706 ; https://digitalcommons.wpi.edu/etd-theses/917

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):

Martinez, Nicolas. “Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere.” 2015. Thesis, Worcester Polytechnic Institute. Accessed September 26, 2020. etd-072915-163706 ; https://digitalcommons.wpi.edu/etd-theses/917.

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

MLA Handbook (7th Edition):

Martinez, Nicolas. “Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere.” 2015. Web. 26 Sep 2020.

Vancouver:

Martinez N. Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere. [Internet] [Thesis]. Worcester Polytechnic Institute; 2015. [cited 2020 Sep 26]. Available from: etd-072915-163706 ; https://digitalcommons.wpi.edu/etd-theses/917.

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

Council of Science Editors:

Martinez N. Feasibility for Orbital Life Extension of a CubeSat Flying in the Lower Thermosphere. [Thesis]. Worcester Polytechnic Institute; 2015. Available from: etd-072915-163706 ; https://digitalcommons.wpi.edu/etd-theses/917

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

28. Olivieri, Steven J. Modular FPGA-Based Software Defined Radio for CubeSats.

Degree: MS, 2011, Worcester Polytechnic Institute

 Digital communications devices designed with application-specific integrated circuit (ASIC) technology suffer from one very significant limitationâ€â€�the integrated circuits are not programmable. Therefore, deploying a new… (more)

Subjects/Keywords: fpga; software-defined radio; cubesat; sdr; radio

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APA (6th Edition):

Olivieri, S. J. (2011). Modular FPGA-Based Software Defined Radio for CubeSats. (Thesis). Worcester Polytechnic Institute. Retrieved from etd-042711-091356 ; https://digitalcommons.wpi.edu/etd-theses/375

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):

Olivieri, Steven J. “Modular FPGA-Based Software Defined Radio for CubeSats.” 2011. Thesis, Worcester Polytechnic Institute. Accessed September 26, 2020. etd-042711-091356 ; https://digitalcommons.wpi.edu/etd-theses/375.

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

MLA Handbook (7th Edition):

Olivieri, Steven J. “Modular FPGA-Based Software Defined Radio for CubeSats.” 2011. Web. 26 Sep 2020.

Vancouver:

Olivieri SJ. Modular FPGA-Based Software Defined Radio for CubeSats. [Internet] [Thesis]. Worcester Polytechnic Institute; 2011. [cited 2020 Sep 26]. Available from: etd-042711-091356 ; https://digitalcommons.wpi.edu/etd-theses/375.

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

Council of Science Editors:

Olivieri SJ. Modular FPGA-Based Software Defined Radio for CubeSats. [Thesis]. Worcester Polytechnic Institute; 2011. Available from: etd-042711-091356 ; https://digitalcommons.wpi.edu/etd-theses/375

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

29. Lu, Ye. CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters.

Degree: MS, 2015, Worcester Polytechnic Institute

 This study presents the overall design of a 3U CubeSat equipped with commercial-off-the shelf hardware, Teflon-fueled micro-Pulsed Plasma Thrusters (µPPT) and an attitude determination and… (more)

Subjects/Keywords: attitude control; CubeSat; pulsed plasma thrusters

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APA (6th Edition):

Lu, Y. (2015). CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters. (Thesis). Worcester Polytechnic Institute. Retrieved from etd-042915-145659 ; https://digitalcommons.wpi.edu/etd-theses/511

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):

Lu, Ye. “CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters.” 2015. Thesis, Worcester Polytechnic Institute. Accessed September 26, 2020. etd-042915-145659 ; https://digitalcommons.wpi.edu/etd-theses/511.

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

MLA Handbook (7th Edition):

Lu, Ye. “CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters.” 2015. Web. 26 Sep 2020.

Vancouver:

Lu Y. CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters. [Internet] [Thesis]. Worcester Polytechnic Institute; 2015. [cited 2020 Sep 26]. Available from: etd-042915-145659 ; https://digitalcommons.wpi.edu/etd-theses/511.

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

Council of Science Editors:

Lu Y. CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters. [Thesis]. Worcester Polytechnic Institute; 2015. Available from: etd-042915-145659 ; https://digitalcommons.wpi.edu/etd-theses/511

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

30. Bailet, Gilles. Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol.

Degree: Docteur es, Énergétique, 2019, Université Paris-Saclay (ComUE)

 Dévoiler les mystères du système solaire pour comprendre les mécanismes de la formation de la Terre, pour rechercher des signes de vie ou pour développer… (more)

Subjects/Keywords: Aérothermodynamiques hypersonique; Rayonnement; Ablation; Instrumentation; Rentrée; CubeSat; Hypersonic aerothermodynamics; Radiation; Ablation; Instrumentation; Reentry; CubeSat

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

APA (6th Edition):

Bailet, G. (2019). Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol. (Doctoral Dissertation). Université Paris-Saclay (ComUE). Retrieved from http://www.theses.fr/2019SACLC008

Chicago Manual of Style (16th Edition):

Bailet, Gilles. “Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol.” 2019. Doctoral Dissertation, Université Paris-Saclay (ComUE). Accessed September 26, 2020. http://www.theses.fr/2019SACLC008.

MLA Handbook (7th Edition):

Bailet, Gilles. “Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol.” 2019. Web. 26 Sep 2020.

Vancouver:

Bailet G. Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol. [Internet] [Doctoral dissertation]. Université Paris-Saclay (ComUE); 2019. [cited 2020 Sep 26]. Available from: http://www.theses.fr/2019SACLC008.

Council of Science Editors:

Bailet G. Radiation and ablation studies for in-flight validation : Étude du Rayonnement et de l’Ablation pour Validation en Vol. [Doctoral Dissertation]. Université Paris-Saclay (ComUE); 2019. Available from: http://www.theses.fr/2019SACLC008

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