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Electrode Geometry Effects in an Electrothermal Plasma Microthruster
Author(s) -
Harrison Raymond King
Publication year - 2018
Language(s) - Uncategorized
Resource type - Dissertations/theses
DOI - 10.15368/theses.2018.73
Subject(s) - aerospace engineering , ion thruster , propellant , spacecraft , plasma , thrust , debye sheath , mechanical engineering , argon , computational fluid dynamics , spacecraft propulsion , electrode , mechanics , physics , propulsion , materials science , engineering , atomic physics , nuclear physics , quantum mechanics

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