A micro-nozzle thruster comprising a micro-nozzle having an inlet at a first end perpendicularly aligned gas supply channel at a first end, and a thruster outlet at a second opposed end; said inlet in fluid communication with a gas supply channel, said gas supply channel perpendicularly aligned with a longitudinal axis of the micro-nozzle; a cathode within the gas supply channel and an anode external to the gas supply channel and proximate to the inlet, so as to create a plasma flow from said gas.
A MICRO-NOZZLE THRUSTER
MIKRODÜSENANTRIEB
PROPULSEUR À MICRO-TUYÈRE
05.04.2017
Patent
Elektronische Ressource
Englisch
MICRO-NOZZLE DESIGN FOR AN ELECTROTHERMAL PLASMA THRUSTER
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