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Real-time in situ determination of inductively coupled power and axi-symmetric model based prediction of heuristic plasma parameters in RF ion thrusters

Volkmar, Chris and Neumann, Andreas and Geile, Christopher and Hannemann, Klaus (2017) Real-time in situ determination of inductively coupled power and axi-symmetric model based prediction of heuristic plasma parameters in RF ion thrusters. XXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen, 2017-03-07 - 2017-03-09, Mühlleithen, Deutschland.

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Official URL: http://web1454.web02.sh.united-host.de/iom/muehlleithen/2017/index.cfm


Item URL in elib:https://elib.dlr.de/119692/
Document Type:Conference or Workshop Item (Speech)
Title:Real-time in situ determination of inductively coupled power and axi-symmetric model based prediction of heuristic plasma parameters in RF ion thrusters
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Volkmar, ChrisUNSPECIFIEDhttps://orcid.org/0000-0002-5038-3834UNSPECIFIED
Neumann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Geile, ChristopherUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:RF ion thrusters, modeling, inductively coupled plasma, power measurement
Event Title:XXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen
Event Location:Mühlleithen, Deutschland
Event Type:Workshop
Event Start Date:7 March 2017
Event End Date:9 March 2017
Organizer:Christian-Albrechts-Universität zu Kiel, Ernst Moritz Arndt Universtiät Greifswald
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 - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old)
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Bachmann, Barbara
Deposited On:27 Jun 2018 15:50
Last Modified:24 Apr 2024 20:23

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