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Investigation of the Magnetic Nozzle Configuration on the ALFVEN Thruster Performance

Chan, Yung-An and Geile, Christopher and Plettenberg, Felix and Schmidt, Jens and Takahashi, Kazunori (2025) Investigation of the Magnetic Nozzle Configuration on the ALFVEN Thruster Performance. In: 39th International Electric Propulsion Conference (IEPC) 2025, pp. 1-12. 39th International Electric Propulsion Conference (IEPC) 2025, 2025-09-14 - 2025-09-19, London, UK.

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Official URL: https://www.imperial.ac.uk/iepc2025/

Abstract

This work investigates the influence of magnetic field topology on the performance of the ALFVEN-4050 RF plasma thruster. Two magnetic configurations were tested: a standard (STD) field and a divergent magnetic nozzle (DMN). Plasma diagnostics using a Langmuir probe and retarding potential analyzer reveal that the DMN configuration yields higher electron temperatures and maintains more stable plume characteristics across varying flow rates, while exhibiting lower plasma density compared to STD. Ion energy distribution function (IEDF) measurements show significantly higher ion beam energies in DMN, indicating enhanced plasma acceleration. Thrust measurements confirm that DMN produces higher thrust and up to three times higher efficiency at low flow rates compared to STD. These findings demonstrate that magnetic nozzle shaping strongly affects power coupling and ion acceleration efficiency, providing a pathway for optimizing electrodeless plasma thrusters for improved performance.

Item URL in elib:https://elib.dlr.de/213133/
Document Type:Conference or Workshop Item (Speech)
Title:Investigation of the Magnetic Nozzle Configuration on the ALFVEN Thruster Performance
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Chan, Yung-Anyung-an.chan (at) dlr.dehttps://orcid.org/0000-0001-5494-0514195385487
Geile, ChristopherChristopher.Geile (at) dlr.deUNSPECIFIEDUNSPECIFIED
Plettenberg, Felixfelix.plettenberg (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schmidt, JensJens.Schmidt (at) dlr.dehttps://orcid.org/0000-0002-2052-8588195385489
Takahashi, Kazunorikazunori.takahashi.e8 (at) tohoku.ac.jp.UNSPECIFIEDUNSPECIFIED
Date:19 September 2025
Journal or Publication Title:39th International Electric Propulsion Conference (IEPC) 2025
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIEDERPSUNSPECIFIEDUNSPECIFIED
Series Name:Online Proceedings
Status:Published
Keywords:Electrodemess plasma thruster, magnetic nozzle, resonant network
Event Title:39th International Electric Propulsion Conference (IEPC) 2025
Event Location:London, UK
Event Type:international Conference
Event Start Date:14 September 2025
Event End Date:19 September 2025
Organizer:International Electric Propulsion Society
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Project Decentralized Energy Supplied Electrical Propulsion
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Chan, Dr.-Ing. Yung-An
Deposited On:28 Oct 2025 14:42
Last Modified:06 May 2026 08:42

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