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A simple and low-cost xenon flow controller applying a heated capillary is proposed and successfully demonstrated. Based on a turbulent assumption, the developed theory is in good agreement with the experiment.
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This page is a summary of: Characterization of a Capillary Flow Controller for Electric Propulsion, Journal of Propulsion and Power, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37726.
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