Plasma properties conditioned by the magnetic throat location in a helicon plasma device

Author:

Vinci Alfio E.1ORCID,Mazouffre Stéphane1ORCID

Affiliation:

1. Institut de Combustion, Aérothermique, Réactivité et Environnement (ICARE), Centre National de la Recherche Scientifique, 1C Avenue de la Recherche Scientifique, 45071 Orléans, France

Funder

European Union Horizon 2020

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Reference54 articles.

1. Space micropropulsion systems for Cubesats and small satellites: From proximate targets to furthermost frontiers

2. J. M. Martínez, D. Rafalskyi, and A. Aanesland, “Development and testing of the NPT30-I2 iodine ion thruster,” in 36th International Electric Propulsion Conference (2019).

3. A. Gurciullo, J. Jarrige, P. Lascombes, and D. Packan, “Experimental performance and plume characterisation of a miniaturised 50W Hall thruster,” in 36th International Electric Propulsion Conference (2019).

4. Perspectives, frontiers, and new horizons for plasma-based space electric propulsion

5. Future Directions for Electric Propulsion Research

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