A CubeSAT Orbital Test Platform for an Electrothermal Plasma Micro-Thruster
As the viability and capability of CubeSats increases, a demand for propulsion systems is becoming apparent. The limitations put forth in the ``CubeSat Design Specifications" and the additional difficulties of low available Size, Weight and Power (SWaP) for propulsion systems aboard CubeSats ha...
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| Format: | Others |
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DigitalCommons@CalPoly
2019
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| Online Access: | https://digitalcommons.calpoly.edu/theses/2034 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3459&context=theses |