Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster
With an increased demand in Cube Satellite (CubeSat) development for low cost science and exploration missions, a push for the development of micro-propulsion technology has emerged, which seeks to increase CubeSat capabilities for novel mission concepts. One type of micro-propulsion system currentl...
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| Format: | Others |
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DigitalCommons@CalPoly
2018
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| Online Access: | https://digitalcommons.calpoly.edu/theses/1961 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3338&context=theses |