Schäfer, Clara and Zorn, Jana and Holste, Kristof and Klar, P. J. (2024) Influences on Langmuir probe measurements by an ECR thruster with magnetic nozzle. In: 23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV, 154, pp. 153-162. Springer Nature. 23. STAB-DGLR-Symposium 2022, 2022-11-09 - 2022-11-10, Berlin, Deutschland. doi: 10.1007/978-3-031-40482-5_15. ISBN 978-3-031-40481-8. ISSN 1612-2909.
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Official URL: https://link.springer.com/book/10.1007/978-3-031-40482-5
Abstract
Ensuring reliability in the measurement and interpretation of plasma diagnostics is essential for characterizing thruster concepts in the uprising field of electric propulsion. Langmuir probes are often used to determine the properties of low temperature plasmas. However, not much research is found on Langmuir probe measurements on electron cyclotron resonance thrusters with magnetic nozzle, especially no detailed studies on variable probe orientations with respect to magnetic field lines. The question arises which differences can be shown in the electron energy distribution regarding the probes orientation and in what way it is possible to interpret probe alignment consequences on determined plasma characteristics. We perform our study as follows: We measure in two orientations, parallel and orthogonal to magnetic field lines, at different operating states of the thruster (variable power and volume flow settings). The Langmuir probe data shows clearly a dependency on the probes orientation. We use the measured ion energy distribution of the retarding potential analyzer as a comparison tool to the determined electron energy distribution of the single Langmuir probe measurements. Due to the determined anisotropic non-Maxwellian distribution mainly visible in parallel orientation we conclude a parallel orientation of Langmuir probes with respect to magnetic field lines is preferable for ECRT with MN.
| Item URL in elib: | https://elib.dlr.de/193625/ | ||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||
| Additional Information: | ISSN 1612-2909 ISSN 1860-0824 (electronic) ISBN 978-3-031-40481-8 ISBN 978-3-031-40482-5 (eBook) | ||||||||||||||||||||||||
| Title: | Influences on Langmuir probe measurements by an ECR thruster with magnetic nozzle | ||||||||||||||||||||||||
| Authors: |
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| Date: | 2024 | ||||||||||||||||||||||||
| Journal or Publication Title: | 23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV | ||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||
| Volume: | 154 | ||||||||||||||||||||||||
| DOI: | 10.1007/978-3-031-40482-5_15 | ||||||||||||||||||||||||
| Page Range: | pp. 153-162 | ||||||||||||||||||||||||
| Editors: |
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| Publisher: | Springer Nature | ||||||||||||||||||||||||
| Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||||||||||||||
| ISSN: | 1612-2909 | ||||||||||||||||||||||||
| ISBN: | 978-3-031-40481-8 | ||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||
| Keywords: | ECRT, magnetic nozzle, Langmuir probe, EEDF | ||||||||||||||||||||||||
| Event Title: | 23. STAB-DGLR-Symposium 2022 | ||||||||||||||||||||||||
| Event Location: | Berlin, Deutschland | ||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||
| Event Start Date: | 9 November 2022 | ||||||||||||||||||||||||
| Event End Date: | 10 November 2022 | ||||||||||||||||||||||||
| Organizer: | STAB/DGLR | ||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||
| HGF - Program: | Space | ||||||||||||||||||||||||
| HGF - Program Themes: | Space Transportation | ||||||||||||||||||||||||
| DLR - Research area: | Raumfahrt | ||||||||||||||||||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||||||||||||||||||
| DLR - Research theme (Project): | R - Reusable Space Systems and Propulsion Technology | ||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Spacecraft, GO | ||||||||||||||||||||||||
| Deposited By: | Schäfer, Clara | ||||||||||||||||||||||||
| Deposited On: | 31 Jul 2024 15:09 | ||||||||||||||||||||||||
| Last Modified: | 31 Jul 2024 17:57 |
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