Abstract
In this communication we report on a combined experimental-numerical activity thas was conducted to assess the antenna-plasma interaction within a Helicon plasma source for space thrusters. The experiment is based on a versatile, re-configurable set-up which allows testing mulitiple thruster configurations under different operating condtions, featuring a high-efficiency RF antenna. The numerical results were opbtained by means of various simulation tools for both RF circuit and antenna-plasma interface analysis; these tools were validated against experimental data. The results helped to improve our understanding of antenna-plasma coupling and the assessment/prediction of the RF system performance.
Original language | Dutch |
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Title of host publication | Proceedings of the AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio |
Pages | 1-26 |
DOIs | |
Publication status | Published - 2014 |
Event | AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio - Cleveland, United States Duration: 28 Jul 2014 → 30 Jul 2014 |
Conference
Conference | AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio |
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Country/Territory | United States |
City | Cleveland |
Period | 28/07/14 → 30/07/14 |