Ion acceleration in expanding plasma in small radio frequency plasma thruster with a magnetic cusp
Author:
Affiliation:
1. Kobe University 1 , Hyogo 657-8501, Japan
2. Japan Air Self-Defense Force 2 , Tokyo 162-8804, Japan
3. Ryukoku University 3 , Shiga 520-2123, Japan
4. Tokyo University of Agriculture and Technology 4 , Tokyo 184-8588, Japan
Abstract
Funder
Japan Society for the Promotion of Science
NIFS Collaboration Research Program
Publisher
AIP Publishing
Subject
Physics and Astronomy (miscellaneous)
Link
https://pubs.aip.org/aip/apl/article-pdf/doi/10.1063/5.0174387/18226292/224101_1_5.0174387.pdf
Reference33 articles.
1. Direct thrust measurements and modelling of a radio-frequency expanding plasma thruster
2. Development of Electrodeless Plasma Thrusters With High-Density Helicon Plasma Sources
3. Helicon-type radiofrequency plasma thrusters and magnetic plasma nozzles
4. Electron Cooling in a Magnetically Expanding Plasma
5. A magnetic nozzle calculation of the force on a plasma
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