Chan, Yung-An und Geile, Christopher und Plettenberg, Felix und Schmidt, Jens und Takahashi, Kazunori (2025) Investigation of the Magnetic Nozzle Configuration on the ALFVEN Thruster Performance. In: 39th International Electric Propulsion Conference (IEPC) 2025, Seiten 1-12. 39th International Electric Propulsion Conference (IEPC) 2025, 2025-09-14 - 2025-09-19, London, UK.
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Offizielle URL: https://www.imperial.ac.uk/iepc2025/
Kurzfassung
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.
| elib-URL des Eintrags: | https://elib.dlr.de/213133/ | ||||||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
| Titel: | Investigation of the Magnetic Nozzle Configuration on the ALFVEN Thruster Performance | ||||||||||||||||||||||||
| Autoren: |
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| Datum: | 19 September 2025 | ||||||||||||||||||||||||
| Erschienen in: | 39th International Electric Propulsion Conference (IEPC) 2025 | ||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||
| Seitenbereich: | Seiten 1-12 | ||||||||||||||||||||||||
| Herausgeber: |
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| Name der Reihe: | Online Proceedings | ||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||
| Stichwörter: | Electrodemess plasma thruster, magnetic nozzle, resonant network | ||||||||||||||||||||||||
| Veranstaltungstitel: | 39th International Electric Propulsion Conference (IEPC) 2025 | ||||||||||||||||||||||||
| Veranstaltungsort: | London, UK | ||||||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
| Veranstaltungsbeginn: | 14 September 2025 | ||||||||||||||||||||||||
| Veranstaltungsende: | 19 September 2025 | ||||||||||||||||||||||||
| Veranstalter : | Imperial College London | ||||||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
| HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||
| HGF - Programmthema: | Technik für Raumfahrtsysteme | ||||||||||||||||||||||||
| DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||
| DLR - Forschungsgebiet: | R SY - Technik für Raumfahrtsysteme | ||||||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | R - Projekt Decentralized Energy supplied Electrical Propulsion | ||||||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge, GO | ||||||||||||||||||||||||
| Hinterlegt von: | Chan, Dr.-Ing. Yung-An | ||||||||||||||||||||||||
| Hinterlegt am: | 28 Okt 2025 14:42 | ||||||||||||||||||||||||
| Letzte Änderung: | 28 Okt 2025 14:42 |
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