Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Small Satellites). Showing records 1 – 30 of 40 total matches.

[1] [2]

Search Limiters

Last 2 Years | English Only

▼ Search Limiters


University of Utah

1. Saberin, Jason Ramin. Optically transparent antennas for small satellites.

Degree: MS;, Electrical & Computer Engineering;, 2010, University of Utah

 In this thesis the placement of antennas on a small satellite's solar cell is studied. The place-ment of antennas is carefully investigated by minimizing the… (more)

Subjects/Keywords: Optically transparent antennas; Small satellites

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Saberin, J. R. (2010). Optically transparent antennas for small satellites. (Masters Thesis). University of Utah. Retrieved from http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/733/rec/844

Chicago Manual of Style (16th Edition):

Saberin, Jason Ramin. “Optically transparent antennas for small satellites.” 2010. Masters Thesis, University of Utah. Accessed January 22, 2021. http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/733/rec/844.

MLA Handbook (7th Edition):

Saberin, Jason Ramin. “Optically transparent antennas for small satellites.” 2010. Web. 22 Jan 2021.

Vancouver:

Saberin JR. Optically transparent antennas for small satellites. [Internet] [Masters thesis]. University of Utah; 2010. [cited 2021 Jan 22]. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/733/rec/844.

Council of Science Editors:

Saberin JR. Optically transparent antennas for small satellites. [Masters Thesis]. University of Utah; 2010. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/733/rec/844


Texas A&M University

2. Graves, John. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 Within the first decade of the 21st century, the aerospace community has seen many more opportunities to launch small spacecraft in the 10 to 100… (more)

Subjects/Keywords: Small satellites; RFIC; downlink communications; spacecraft; university satellites

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Graves, J. (2012). Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387

Chicago Manual of Style (16th Edition):

Graves, John. “Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.” 2012. Masters Thesis, Texas A&M University. Accessed January 22, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387.

MLA Handbook (7th Edition):

Graves, John. “Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits.” 2012. Web. 22 Jan 2021.

Vancouver:

Graves J. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387.

Council of Science Editors:

Graves J. Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-12-10387


Cornell University

3. Zeledon, Rodrigo. Electrolysis Propulsion For Small-Scale Spacecraft.

Degree: PhD, Aerospace Engineering, 2015, Cornell University

 In the past decade, CubeSats have revolutionized small spacecraft missions. These miniature satellites began as educational projects but have lowered the bar for access to… (more)

Subjects/Keywords: Electrolysis propulsion; Small satellites; Spacecraft dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zeledon, R. (2015). Electrolysis Propulsion For Small-Scale Spacecraft. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/40701

Chicago Manual of Style (16th Edition):

Zeledon, Rodrigo. “Electrolysis Propulsion For Small-Scale Spacecraft.” 2015. Doctoral Dissertation, Cornell University. Accessed January 22, 2021. http://hdl.handle.net/1813/40701.

MLA Handbook (7th Edition):

Zeledon, Rodrigo. “Electrolysis Propulsion For Small-Scale Spacecraft.” 2015. Web. 22 Jan 2021.

Vancouver:

Zeledon R. Electrolysis Propulsion For Small-Scale Spacecraft. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1813/40701.

Council of Science Editors:

Zeledon R. Electrolysis Propulsion For Small-Scale Spacecraft. [Doctoral Dissertation]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40701

4. Komus, Alastair. Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites.

Degree: MS, Space Studies, 2017, University of North Dakota

  Out-of-autoclave vacuum-bagged-only (VBO) processing is capable of producing lower cost composite primary structures for small satellites than autoclave processing. However, the outgassing performance of… (more)

Subjects/Keywords: Composites; Outgassing; Out-of-Autoclave; Small Satellites

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Komus, A. (2017). Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/2254

Chicago Manual of Style (16th Edition):

Komus, Alastair. “Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites.” 2017. Masters Thesis, University of North Dakota. Accessed January 22, 2021. https://commons.und.edu/theses/2254.

MLA Handbook (7th Edition):

Komus, Alastair. “Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites.” 2017. Web. 22 Jan 2021.

Vancouver:

Komus A. Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites. [Internet] [Masters thesis]. University of North Dakota; 2017. [cited 2021 Jan 22]. Available from: https://commons.und.edu/theses/2254.

Council of Science Editors:

Komus A. Outgassing Of Out-Of-Autoclave Composite Primary Structures For Small Satellites. [Masters Thesis]. University of North Dakota; 2017. Available from: https://commons.und.edu/theses/2254


University of Houston

5. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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. (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 January 22, 2021. http://hdl.handle.net/10657/1553.

MLA Handbook (7th Edition):

Phadnis, Mandar 1988-. “Feedback Control of CubeSat for Attitude and Trajectory Corrections.” 2013. Web. 22 Jan 2021.

Vancouver:

Phadnis M1. Feedback Control of CubeSat for Attitude and Trajectory Corrections. [Internet] [Masters thesis]. University of Houston; 2013. [cited 2021 Jan 22]. 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


Cranfield University

6. Ayad, A. An evaluation of small satellite technology transfer and capability-building in Algeria.

Degree: 2018, Cranfield University

 The potential for satellite technology to make an essential contribution to socio-economic development has been recognised by the international community since the onset of space… (more)

Subjects/Keywords: Small satellites; Developing countries; Technology transfer

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ayad, A. (2018). An evaluation of small satellite technology transfer and capability-building in Algeria. (Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/15295

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):

Ayad, A. “An evaluation of small satellite technology transfer and capability-building in Algeria.” 2018. Thesis, Cranfield University. Accessed January 22, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/15295.

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

MLA Handbook (7th Edition):

Ayad, A. “An evaluation of small satellite technology transfer and capability-building in Algeria.” 2018. Web. 22 Jan 2021.

Vancouver:

Ayad A. An evaluation of small satellite technology transfer and capability-building in Algeria. [Internet] [Thesis]. Cranfield University; 2018. [cited 2021 Jan 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/15295.

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

Council of Science Editors:

Ayad A. An evaluation of small satellite technology transfer and capability-building in Algeria. [Thesis]. Cranfield University; 2018. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/15295

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


University of Manchester

7. Crisp, Nicholas Husayn. A Methodology for the Integrated Design of Small Satellite Constellation Deployment.

Degree: 2016, University of Manchester

 A growing interest in distributed systems of small satellites has recently emerged due to their ability to perform a variety of new mission types, increasing… (more)

Subjects/Keywords: Small satellites; Nanosatellites; Access to orbit; Genetic algorithm; Multiobjective optimisation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crisp, N. H. (2016). A Methodology for the Integrated Design of Small Satellite Constellation Deployment. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302321

Chicago Manual of Style (16th Edition):

Crisp, Nicholas Husayn. “A Methodology for the Integrated Design of Small Satellite Constellation Deployment.” 2016. Doctoral Dissertation, University of Manchester. Accessed January 22, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302321.

MLA Handbook (7th Edition):

Crisp, Nicholas Husayn. “A Methodology for the Integrated Design of Small Satellite Constellation Deployment.” 2016. Web. 22 Jan 2021.

Vancouver:

Crisp NH. A Methodology for the Integrated Design of Small Satellite Constellation Deployment. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 22]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302321.

Council of Science Editors:

Crisp NH. A Methodology for the Integrated Design of Small Satellite Constellation Deployment. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302321


University of Toronto

8. Elliott, Jennifer. The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites.

Degree: 2014, University of Toronto

The main appeal of small satellites is that they are capable of fulfilling many of the same tasks as larger satellites, with lower development and… (more)

Subjects/Keywords: nanosatellites; passive thermal control; small satellites; thermal control; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Elliott, J. (2014). The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/67848

Chicago Manual of Style (16th Edition):

Elliott, Jennifer. “The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites.” 2014. Masters Thesis, University of Toronto. Accessed January 22, 2021. http://hdl.handle.net/1807/67848.

MLA Handbook (7th Edition):

Elliott, Jennifer. “The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites.” 2014. Web. 22 Jan 2021.

Vancouver:

Elliott J. The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1807/67848.

Council of Science Editors:

Elliott J. The Thermal Design and Analysis of the CanX-4/-5 and NEMO-AM Nanosatellites. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/67848


University of Toronto

9. Fournier, Marc. Attitude Determination and Control Hardware Development for Small Satellites.

Degree: 2011, University of Toronto

The development of a small spacecraft attitude determination and control subsystem is described. This subsystem is part of The Space Flight Laboratory's Generic Nanosatellite Bus.… (more)

Subjects/Keywords: Attitude Determination and Control Hardware Development for Small Satellites; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Fournier, M. (2011). Attitude Determination and Control Hardware Development for Small Satellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/29545

Chicago Manual of Style (16th Edition):

Fournier, Marc. “Attitude Determination and Control Hardware Development for Small Satellites.” 2011. Masters Thesis, University of Toronto. Accessed January 22, 2021. http://hdl.handle.net/1807/29545.

MLA Handbook (7th Edition):

Fournier, Marc. “Attitude Determination and Control Hardware Development for Small Satellites.” 2011. Web. 22 Jan 2021.

Vancouver:

Fournier M. Attitude Determination and Control Hardware Development for Small Satellites. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1807/29545.

Council of Science Editors:

Fournier M. Attitude Determination and Control Hardware Development for Small Satellites. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/29545


University of Toronto

10. Wheeler, Clyde Bennet. Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites.

Degree: 2017, University of Toronto

Commercial off-the-shelf camera technology is frequently adapted for use onboard small satellites to aid in the validation of deployment mechanisms. Commercial off-the-shelf cameras are not… (more)

Subjects/Keywords: imaging science; microsatellites; nanosatellites; radiometric calibration; radiometry; small satellites; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wheeler, C. B. (2017). Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/77909

Chicago Manual of Style (16th Edition):

Wheeler, Clyde Bennet. “Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites.” 2017. Masters Thesis, University of Toronto. Accessed January 22, 2021. http://hdl.handle.net/1807/77909.

MLA Handbook (7th Edition):

Wheeler, Clyde Bennet. “Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites.” 2017. Web. 22 Jan 2021.

Vancouver:

Wheeler CB. Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1807/77909.

Council of Science Editors:

Wheeler CB. Adaptation of Commercial Off-the-shelf Camera Technology for Deployment Imaging and Inspection on Small Satellites. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/77909

11. Bergsrud, Corey Marvin. Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna.

Degree: PhD, Electrical Engineering, 2016, University of North Dakota

  Space solar power satellite (SSPS) systems is the concept of placing large satellite into geostationary Earth orbit (GEO) to harvest and convert massive amounts… (more)

Subjects/Keywords: Microwave Wireless Power; Modern Small Satellites; Space Rectenna; Space Solar Power

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bergsrud, C. M. (2016). Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna. (Doctoral Dissertation). University of North Dakota. Retrieved from https://commons.und.edu/theses/1875

Chicago Manual of Style (16th Edition):

Bergsrud, Corey Marvin. “Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna.” 2016. Doctoral Dissertation, University of North Dakota. Accessed January 22, 2021. https://commons.und.edu/theses/1875.

MLA Handbook (7th Edition):

Bergsrud, Corey Marvin. “Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna.” 2016. Web. 22 Jan 2021.

Vancouver:

Bergsrud CM. Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna. [Internet] [Doctoral dissertation]. University of North Dakota; 2016. [cited 2021 Jan 22]. Available from: https://commons.und.edu/theses/1875.

Council of Science Editors:

Bergsrud CM. Space Solar Power Satellite Systems, Modern Small Satellites, And Space Rectenna. [Doctoral Dissertation]. University of North Dakota; 2016. Available from: https://commons.und.edu/theses/1875

12. Crisp, Nicholas Husayn. A methodology for the integrated design of small satellite constellation deployment.

Degree: PhD, 2016, University of Manchester

 A growing interest in distributed systems of small satellites has recently emerged due to their ability to perform a variety of new mission types, increasing… (more)

Subjects/Keywords: 629.43; Small satellites; Nanosatellites; Access to orbit; Genetic algorithm; Multiobjective optimisation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crisp, N. H. (2016). A methodology for the integrated design of small satellite constellation deployment. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/a-methodology-for-the-integrated-design-of-small-satellite-constellation-deployment(46968b9a-6151-4e35-905d-e1b9b7f0609a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701132

Chicago Manual of Style (16th Edition):

Crisp, Nicholas Husayn. “A methodology for the integrated design of small satellite constellation deployment.” 2016. Doctoral Dissertation, University of Manchester. Accessed January 22, 2021. https://www.research.manchester.ac.uk/portal/en/theses/a-methodology-for-the-integrated-design-of-small-satellite-constellation-deployment(46968b9a-6151-4e35-905d-e1b9b7f0609a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701132.

MLA Handbook (7th Edition):

Crisp, Nicholas Husayn. “A methodology for the integrated design of small satellite constellation deployment.” 2016. Web. 22 Jan 2021.

Vancouver:

Crisp NH. A methodology for the integrated design of small satellite constellation deployment. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 22]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/a-methodology-for-the-integrated-design-of-small-satellite-constellation-deployment(46968b9a-6151-4e35-905d-e1b9b7f0609a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701132.

Council of Science Editors:

Crisp NH. A methodology for the integrated design of small satellite constellation deployment. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/a-methodology-for-the-integrated-design-of-small-satellite-constellation-deployment(46968b9a-6151-4e35-905d-e1b9b7f0609a).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701132

13. -4224-5412. Design and testing of a 3D printed propulsion system for small satellites.

Degree: MSin Engineering, Aerospace Engineering, 2015, University of Texas – Austin

 A cold gas propulsion system for small spacecraft orbital maneuvers was developed by the University of Texas at Austin's Texas Spacecraft Laboratory. The thruster will… (more)

Subjects/Keywords: Small satellites; Micropropulsion

…xii . 52 . 54 . 55 . 56 . 57 . 60 . 61 . 62 Chapter 1 Introduction Small satellites are… …greatly in capability. One area of capability that small satellites are developing is propulsion… …systems. The development of miniature propulsion systems will enable small satellites to… …into seven chapters. Chapter 2 explains the motivation for small satellites in general, and… …development times of small satellites to reduce the cost of space-based services [2]. In… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

-4224-5412. (2015). Design and testing of a 3D printed propulsion system for small satellites. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31714

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-4224-5412. “Design and testing of a 3D printed propulsion system for small satellites.” 2015. Masters Thesis, University of Texas – Austin. Accessed January 22, 2021. http://hdl.handle.net/2152/31714.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-4224-5412. “Design and testing of a 3D printed propulsion system for small satellites.” 2015. Web. 22 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-4224-5412. Design and testing of a 3D printed propulsion system for small satellites. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/2152/31714.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-4224-5412. Design and testing of a 3D printed propulsion system for small satellites. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31714

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Universidade do Rio Grande do Sul

14. Guareschi, William do Nascimento. Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável.

Degree: 2015, Universidade do Rio Grande do Sul

O uso de pequenos satélites tem aumentado substancialmente nos últimos anos devido ao custo reduzido de desenvolvimento e lançamento, assim como pela flexibilidade oferecida pela… (more)

Subjects/Keywords: Microeletrônica; Programmable logic devices; Small satellites; Device interfaces; Payloads tests and control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Guareschi, W. d. N. (2015). Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável. (Thesis). Universidade do Rio Grande do Sul. Retrieved from http://hdl.handle.net/10183/141242

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):

Guareschi, William do Nascimento. “Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável.” 2015. Thesis, Universidade do Rio Grande do Sul. Accessed January 22, 2021. http://hdl.handle.net/10183/141242.

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

MLA Handbook (7th Edition):

Guareschi, William do Nascimento. “Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável.” 2015. Web. 22 Jan 2021.

Vancouver:

Guareschi WdN. Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável. [Internet] [Thesis]. Universidade do Rio Grande do Sul; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10183/141242.

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

Council of Science Editors:

Guareschi WdN. Desenvolvimento de uma plataforma para teste e controle de cargas-úteis baseada em arquitetura reconfigurável. [Thesis]. Universidade do Rio Grande do Sul; 2015. Available from: http://hdl.handle.net/10183/141242

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


Cornell University

15. Garcia Buzzi, Pau. Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission.

Degree: M.S., Aerospace Engineering, Aerospace Engineering, 2018, Cornell University

 The orbit and constellation design process for Earth observation missions is complex and it involves trades between different metrics such as mission lifetime, instrument performance,… (more)

Subjects/Keywords: Constellation design; Coverage metrics; Mission analysis; Orbit selection; Satellite; Small satellites; Aerospace engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Garcia Buzzi, P. (2018). Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission. (Masters Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/59601

Chicago Manual of Style (16th Edition):

Garcia Buzzi, Pau. “Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission.” 2018. Masters Thesis, Cornell University. Accessed January 22, 2021. http://hdl.handle.net/1813/59601.

MLA Handbook (7th Edition):

Garcia Buzzi, Pau. “Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission.” 2018. Web. 22 Jan 2021.

Vancouver:

Garcia Buzzi P. Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission. [Internet] [Masters thesis]. Cornell University; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1813/59601.

Council of Science Editors:

Garcia Buzzi P. Assessment of Constellation Designs for Earth observation: Application to the TROPICS mission. [Masters Thesis]. Cornell University; 2018. Available from: http://hdl.handle.net/1813/59601


Stellenbosch University

16. Junaid, Muhammad. The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite.

Degree: MEng, Electrical and Electronic Engineering, 2015, Stellenbosch University

ENGLISH ABSTRACT: The launch costs for satellites are extraordinarily high. This emphasizes the importance of thorough unit and subsystem level testing to minimize the risk… (more)

Subjects/Keywords: Hardware-in-the-loop (HIL) platform  – Development; Small satellites  – Control testing; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Junaid, M. (2015). The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/97881

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):

Junaid, Muhammad. “The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite.” 2015. Thesis, Stellenbosch University. Accessed January 22, 2021. http://hdl.handle.net/10019.1/97881.

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

MLA Handbook (7th Edition):

Junaid, Muhammad. “The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite.” 2015. Web. 22 Jan 2021.

Vancouver:

Junaid M. The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite. [Internet] [Thesis]. Stellenbosch University; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10019.1/97881.

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

Council of Science Editors:

Junaid M. The development of a hardware-in-the-loop platform for the attitude determination and control testing of a small satellite. [Thesis]. Stellenbosch University; 2015. Available from: http://hdl.handle.net/10019.1/97881

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


Brno University of Technology

17. Zíka, Jakub. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.

Degree: 2020, Brno University of Technology

 This thesis is focused on stiffness optimization of small satellite carrying structure - the Dispenser. The first chapter is an introduction to the European space… (more)

Subjects/Keywords: nosič satelitů; optimalizace; metoda konečných prvků; small satellites Dispenser; optimization; finite element method

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zíka, J. (2020). Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/193027

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):

Zíka, Jakub. “Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.” 2020. Thesis, Brno University of Technology. Accessed January 22, 2021. http://hdl.handle.net/11012/193027.

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

MLA Handbook (7th Edition):

Zíka, Jakub. “Optimalizace nosiče satelitů: Small satellite dispenser structural optimization.” 2020. Web. 22 Jan 2021.

Vancouver:

Zíka J. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/11012/193027.

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

Council of Science Editors:

Zíka J. Optimalizace nosiče satelitů: Small satellite dispenser structural optimization. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/193027

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

18. Azari, Pouyan. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.

Degree: Electrical and Space Engineering, 2017, Luleå University of Technology

Cubesats are picosatellites that have a mass of less than 1.3kg and have a shape of acube. As a result of their low cost… (more)

Subjects/Keywords: Orbital mechanics; astrodynamics; small satellites; orbit control; Aerospace Engineering; Rymd- och flygteknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Azari, P. (2017). An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409

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):

Azari, Pouyan. “An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.” 2017. Thesis, Luleå University of Technology. Accessed January 22, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409.

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

MLA Handbook (7th Edition):

Azari, Pouyan. “An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit.” 2017. Web. 22 Jan 2021.

Vancouver:

Azari P. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2021 Jan 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409.

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

Council of Science Editors:

Azari P. An Orbit Control System for UWE-4 Using the High Fidelity Simulation Tool Orekit. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61409

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


Cal Poly

19. Hallak, Yanina Soledad. DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  CubeSats, specially the 6U standard, is nowadays the tendency where many developers point towards. The upscaling size of the standard and payloads entail the… (more)

Subjects/Keywords: CubeSat; Random Vibration; Mechanical Shock; Composite Materials; Finite Element Analysis; Small Satellites; Structures and Materials

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hallak, Y. S. (2016). DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1572 ; 10.15368/theses.2016.49

Chicago Manual of Style (16th Edition):

Hallak, Yanina Soledad. “DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT.” 2016. Masters Thesis, Cal Poly. Accessed January 22, 2021. https://digitalcommons.calpoly.edu/theses/1572 ; 10.15368/theses.2016.49.

MLA Handbook (7th Edition):

Hallak, Yanina Soledad. “DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT.” 2016. Web. 22 Jan 2021.

Vancouver:

Hallak YS. DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Jan 22]. Available from: https://digitalcommons.calpoly.edu/theses/1572 ; 10.15368/theses.2016.49.

Council of Science Editors:

Hallak YS. DESIGN, MANUFACTURE, DYNAMIC TESTING, AND FINITE ELEMENT ANALYSIS OF A COMPOSITE 6U CUBESAT. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1572 ; 10.15368/theses.2016.49


University of Texas – Austin

20. Lum, Annie Megan. Examining differential drag control in a full system simulation.

Degree: MSin Engineering, Aerospace Engineering, 2011, University of Texas – Austin

 Differential drag controllers have been examined in the context of a full system simulation of a target/chaser pair of spacecraft in low Earth orbit. An… (more)

Subjects/Keywords: Differential drag control; Relative state estimation; Measurement simulation; Control optimization; Small satellites

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lum, A. M. (2011). Examining differential drag control in a full system simulation. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-12-4669

Chicago Manual of Style (16th Edition):

Lum, Annie Megan. “Examining differential drag control in a full system simulation.” 2011. Masters Thesis, University of Texas – Austin. Accessed January 22, 2021. http://hdl.handle.net/2152/ETD-UT-2011-12-4669.

MLA Handbook (7th Edition):

Lum, Annie Megan. “Examining differential drag control in a full system simulation.” 2011. Web. 22 Jan 2021.

Vancouver:

Lum AM. Examining differential drag control in a full system simulation. [Internet] [Masters thesis]. University of Texas – Austin; 2011. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-12-4669.

Council of Science Editors:

Lum AM. Examining differential drag control in a full system simulation. [Masters Thesis]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-12-4669


University of Kentucky

21. Lim, Timothy M. A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT.

Degree: 2016, University of Kentucky

Small satellites and CubeSats have established themselves within the aerospace community because of their low cost and high return on investment. Many CubeSats are developed… (more)

Subjects/Keywords: Small Satellites; CubeSats; Electrical Power System; Direct Energy Transfer; Distributed Power System; Electrical and Electronics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lim, T. M. (2016). A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/ece_etds/90

Chicago Manual of Style (16th Edition):

Lim, Timothy M. “A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT.” 2016. Masters Thesis, University of Kentucky. Accessed January 22, 2021. https://uknowledge.uky.edu/ece_etds/90.

MLA Handbook (7th Edition):

Lim, Timothy M. “A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT.” 2016. Web. 22 Jan 2021.

Vancouver:

Lim TM. A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT. [Internet] [Masters thesis]. University of Kentucky; 2016. [cited 2021 Jan 22]. Available from: https://uknowledge.uky.edu/ece_etds/90.

Council of Science Editors:

Lim TM. A MODULAR ELECTRICAL POWER SYSTEM ARCHITECTURE FOR SMALL SPACECRAFT. [Masters Thesis]. University of Kentucky; 2016. Available from: https://uknowledge.uky.edu/ece_etds/90


Cal Poly

22. Ralph, Alyssa M. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  With the rise of CubeSats and the demonstration of their many space applications, there is interest in interplanetary CubeSats to act for example as… (more)

Subjects/Keywords: small satellites; planetary; systems engineering; mission architecture; Systems Engineering and Multidisciplinary Design Optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ralph, A. M. (2020). Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2209

Chicago Manual of Style (16th Edition):

Ralph, Alyssa M. “Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.” 2020. Masters Thesis, Cal Poly. Accessed January 22, 2021. https://digitalcommons.calpoly.edu/theses/2209.

MLA Handbook (7th Edition):

Ralph, Alyssa M. “Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.” 2020. Web. 22 Jan 2021.

Vancouver:

Ralph AM. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Jan 22]. Available from: https://digitalcommons.calpoly.edu/theses/2209.

Council of Science Editors:

Ralph AM. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2209


Cal Poly

23. Harper, James M. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  The research presented provides an overview of a 1U+ form factor propulsion system design developed for the Cal Poly CubeSat Laboratory (CPCL). This design… (more)

Subjects/Keywords: Micro-propulsion; Small Satellites; Space Environment; CubeSat Design Specification; Systems Engineering and Multidisciplinary Design Optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Harper, J. M. (2020). Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2218

Chicago Manual of Style (16th Edition):

Harper, James M. “Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.” 2020. Masters Thesis, Cal Poly. Accessed January 22, 2021. https://digitalcommons.calpoly.edu/theses/2218.

MLA Handbook (7th Edition):

Harper, James M. “Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.” 2020. Web. 22 Jan 2021.

Vancouver:

Harper JM. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Jan 22]. Available from: https://digitalcommons.calpoly.edu/theses/2218.

Council of Science Editors:

Harper JM. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2218


University of Florida

24. Hansoge, Amrith Nagesh. Force Response and Stability of Deployable Mechanisms for Small Satellites.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2014, University of Florida

 In the past, deployable mechanisms for large satellites were developed and over time, highly efficient and multi-featured deployable structures were witnessed. However, with concerns over… (more)

Subjects/Keywords: Artificial satellites; Jacobians; Kinematics; Matrices; Mechanical forces; Mechanical springs; Simulations; Software; Spring constant; Stiffness; deployablemechanisms  – equilibrium  – equilibriumstability  – force  – forceresponse  – incremental  – response  – rotational  – rotationalsprings  – satellites  – small  – smallsatellites  – stability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hansoge, A. N. (2014). Force Response and Stability of Deployable Mechanisms for Small Satellites. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0047261

Chicago Manual of Style (16th Edition):

Hansoge, Amrith Nagesh. “Force Response and Stability of Deployable Mechanisms for Small Satellites.” 2014. Masters Thesis, University of Florida. Accessed January 22, 2021. https://ufdc.ufl.edu/UFE0047261.

MLA Handbook (7th Edition):

Hansoge, Amrith Nagesh. “Force Response and Stability of Deployable Mechanisms for Small Satellites.” 2014. Web. 22 Jan 2021.

Vancouver:

Hansoge AN. Force Response and Stability of Deployable Mechanisms for Small Satellites. [Internet] [Masters thesis]. University of Florida; 2014. [cited 2021 Jan 22]. Available from: https://ufdc.ufl.edu/UFE0047261.

Council of Science Editors:

Hansoge AN. Force Response and Stability of Deployable Mechanisms for Small Satellites. [Masters Thesis]. University of Florida; 2014. Available from: https://ufdc.ufl.edu/UFE0047261


Luleå University of Technology

25. Conijn, Eline. Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent.

Degree: 2015, Luleå University of Technology

This report explores the feasibility of a small satellite constellation used for disaster managementin India. It shows that a small satellite constellation for the… (more)

Subjects/Keywords: Technology; small satellites; disaster management; satellite constellation; India; SAR; optical sizing; MATLAB; cloud cover visibility; Teknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Conijn, E. (2015). Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-58765

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):

Conijn, Eline. “Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent.” 2015. Thesis, Luleå University of Technology. Accessed January 22, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-58765.

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

MLA Handbook (7th Edition):

Conijn, Eline. “Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent.” 2015. Web. 22 Jan 2021.

Vancouver:

Conijn E. Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent. [Internet] [Thesis]. Luleå University of Technology; 2015. [cited 2021 Jan 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-58765.

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

Council of Science Editors:

Conijn E. Phase-0 study of a Disaster Management Satellite Constellation with a Focus on the Indian Subcontinent. [Thesis]. Luleå University of Technology; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-58765

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


Cape Peninsula University of Technology

26. Davids, Vernon Pete. Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites .

Degree: 2019, Cape Peninsula University of Technology

 This dissertation presents a concept for a compact, low-profile, integrated solar panel antenna for use on small satellites in low Earth orbit. To date, the… (more)

Subjects/Keywords: Integrated solar panel antenna; dielectric resonator antenna; transparent antenna; small satellites; beam-steering; Yagi-Uda array

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Davids, V. P. (2019). Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/3044

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):

Davids, Vernon Pete. “Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites .” 2019. Thesis, Cape Peninsula University of Technology. Accessed January 22, 2021. http://etd.cput.ac.za/handle/20.500.11838/3044.

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

MLA Handbook (7th Edition):

Davids, Vernon Pete. “Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites .” 2019. Web. 22 Jan 2021.

Vancouver:

Davids VP. Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites . [Internet] [Thesis]. Cape Peninsula University of Technology; 2019. [cited 2021 Jan 22]. Available from: http://etd.cput.ac.za/handle/20.500.11838/3044.

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

Council of Science Editors:

Davids VP. Design and Implementation of an Integrated Solar Panel Antenna for Small Satellites . [Thesis]. Cape Peninsula University of Technology; 2019. Available from: http://etd.cput.ac.za/handle/20.500.11838/3044

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


University of Kentucky

27. Erb, Daniel Martin. EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT.

Degree: 2011, University of Kentucky

 The unique environment of CubeSat and small satellite missions allows certain accepted paradigms of the larger satellite world to be investigated in order to trade… (more)

Subjects/Keywords: Small Satellites; Power Systems; Solar Arrays; Peak Power Tracking; Direct Energy Transfer; Electrical and Computer Engineering; Electrical and Electronics; Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Erb, D. M. (2011). EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/gradschool_theses/656

Chicago Manual of Style (16th Edition):

Erb, Daniel Martin. “EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT.” 2011. Masters Thesis, University of Kentucky. Accessed January 22, 2021. https://uknowledge.uky.edu/gradschool_theses/656.

MLA Handbook (7th Edition):

Erb, Daniel Martin. “EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT.” 2011. Web. 22 Jan 2021.

Vancouver:

Erb DM. EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT. [Internet] [Masters thesis]. University of Kentucky; 2011. [cited 2021 Jan 22]. Available from: https://uknowledge.uky.edu/gradschool_theses/656.

Council of Science Editors:

Erb DM. EVALUATING THE EFFECTIVENESS OF PEAK POWER TRACKING TECHNOLOGIES FOR SOLAR ARRAYS ON SMALL SPACECRAFT. [Masters Thesis]. University of Kentucky; 2011. Available from: https://uknowledge.uky.edu/gradschool_theses/656


University of Kentucky

28. Torabi, Naseem M. Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays.

Degree: 2013, University of Kentucky

 Body mounted germanium substrate solar cell arrays form the faces of many small satellite designs to provide the primary power source on orbit. High efficiency… (more)

Subjects/Keywords: Solar Cells; Solar Cell Arrays; Circuit Board Assembly; Material Testing; Small Satellites; Electronic Devices and Semiconductor Manufacturing; Structures and Materials

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Torabi, N. M. (2013). Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/ece_etds/22

Chicago Manual of Style (16th Edition):

Torabi, Naseem M. “Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays.” 2013. Masters Thesis, University of Kentucky. Accessed January 22, 2021. https://uknowledge.uky.edu/ece_etds/22.

MLA Handbook (7th Edition):

Torabi, Naseem M. “Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays.” 2013. Web. 22 Jan 2021.

Vancouver:

Torabi NM. Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays. [Internet] [Masters thesis]. University of Kentucky; 2013. [cited 2021 Jan 22]. Available from: https://uknowledge.uky.edu/ece_etds/22.

Council of Science Editors:

Torabi NM. Materials Selection and Processing Techniques for Small Spacecraft Solar Cell Arrays. [Masters Thesis]. University of Kentucky; 2013. Available from: https://uknowledge.uky.edu/ece_etds/22


York University

29. Podmore, Hugh Dennis. Subwavelength Antireflection For Space Applications.

Degree: MSc -MS, Earth & Space Science, 2015, York University

 In this research the potential for CubeSat power-budget enhancement through the application of bio-mimetic subwavelength antireflective nanostructures to solar cell coverglass is investigated. Antireflective nanostructures… (more)

Subjects/Keywords: Nanotechnology; Physics; Aerospace engineering; subwavelength antirefflection; moth eye antireflection; solar cell; light trapping; photonics; photovoltaics; CubeSats; small satellites; satellites; microfabrication; nanofabrication; reactive ion etching; rigorous coupled wave analysis; solar cell enhancement; refractive index engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Podmore, H. D. (2015). Subwavelength Antireflection For Space Applications. (Masters Thesis). York University. Retrieved from http://hdl.handle.net/10315/30723

Chicago Manual of Style (16th Edition):

Podmore, Hugh Dennis. “Subwavelength Antireflection For Space Applications.” 2015. Masters Thesis, York University. Accessed January 22, 2021. http://hdl.handle.net/10315/30723.

MLA Handbook (7th Edition):

Podmore, Hugh Dennis. “Subwavelength Antireflection For Space Applications.” 2015. Web. 22 Jan 2021.

Vancouver:

Podmore HD. Subwavelength Antireflection For Space Applications. [Internet] [Masters thesis]. York University; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10315/30723.

Council of Science Editors:

Podmore HD. Subwavelength Antireflection For Space Applications. [Masters Thesis]. York University; 2015. Available from: http://hdl.handle.net/10315/30723


North Carolina State University

30. Diwan, Maitrik Yogesh. Methodology for Analyzing Complex Algorithms for Small Satellites.

Degree: MS, Computer Engineering, 2007, North Carolina State University

Subjects/Keywords: FPGA; small satellites; DSP; hardware-software co-design; Cubesat; methodology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Diwan, M. Y. (2007). Methodology for Analyzing Complex Algorithms for Small Satellites. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/675

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):

Diwan, Maitrik Yogesh. “Methodology for Analyzing Complex Algorithms for Small Satellites.” 2007. Thesis, North Carolina State University. Accessed January 22, 2021. http://www.lib.ncsu.edu/resolver/1840.16/675.

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

MLA Handbook (7th Edition):

Diwan, Maitrik Yogesh. “Methodology for Analyzing Complex Algorithms for Small Satellites.” 2007. Web. 22 Jan 2021.

Vancouver:

Diwan MY. Methodology for Analyzing Complex Algorithms for Small Satellites. [Internet] [Thesis]. North Carolina State University; 2007. [cited 2021 Jan 22]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/675.

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

Council of Science Editors:

Diwan MY. Methodology for Analyzing Complex Algorithms for Small Satellites. [Thesis]. North Carolina State University; 2007. Available from: http://www.lib.ncsu.edu/resolver/1840.16/675

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

[1] [2]

.