Hey, Franz and Brandt, Tim and Kornfeld, Günter and Braxmaier, Claus and Tajmar, Martin and Johann, Ulrich (2015) Downscaling a HEMPT to micro-Newton Thrust levels: current status and latest results. Conference of 30th International Symposium on Space Technology and Science,, 04.-10.07.2015, Hyogo-Kobe, Japan.
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Abstract
Space, Germany Since 2009 Airbus DS Space Systems, Friedrichshafen, has been investigating Electric Propulsion (EP) systems for high precision attitude and position control of spacecrafts. As a start, an experimental measurement campaign to demonstrate the feasibility of down scaling the High Efficiency Multistage Plasma Thruster (HEMPT), developed by Thales at Ulm in Germany, to the micro-Newton thrust level was initiated in close cooperation with university research groups. The HEMPT is potentially an attractive micro-Newton thruster concept because of the unique advantages of the HEMPT principle, e.g. nearly erosion-free operation and simple system and interface design with just one high voltage supply and one mass flow controller. We designed a next generation μHEMPT with a thrust range between 50 μN to 500 μN, a specific inpuls of more than 2000 s, a divergence efficiency of more than 80% and a mass efficiency of around 70% . The proceeding will wrap up the thruster design and key parameters of the thruster and the performed measurements will be summarised
Item URL in elib: | https://elib.dlr.de/103476/ | |||||||||||||||||||||
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Document Type: | Conference or Workshop Item (Speech) | |||||||||||||||||||||
Title: | Downscaling a HEMPT to micro-Newton Thrust levels: current status and latest results | |||||||||||||||||||||
Authors: |
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Date: | 2015 | |||||||||||||||||||||
Refereed publication: | No | |||||||||||||||||||||
Open Access: | No | |||||||||||||||||||||
Gold Open Access: | No | |||||||||||||||||||||
In SCOPUS: | No | |||||||||||||||||||||
In ISI Web of Science: | No | |||||||||||||||||||||
Status: | Published | |||||||||||||||||||||
Keywords: | HEMPT, electric propulsion, micro-Newton thruster, thrust balance, heterodyne interferometer | |||||||||||||||||||||
Event Title: | Conference of 30th International Symposium on Space Technology and Science, | |||||||||||||||||||||
Event Location: | Hyogo-Kobe, Japan | |||||||||||||||||||||
Event Type: | international Conference | |||||||||||||||||||||
Event Dates: | 04.-10.07.2015 | |||||||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | |||||||||||||||||||||
HGF - Program: | Space | |||||||||||||||||||||
HGF - Program Themes: | other | |||||||||||||||||||||
DLR - Research area: | Raumfahrt | |||||||||||||||||||||
DLR - Program: | R - no assignment | |||||||||||||||||||||
DLR - Research theme (Project): | R - no assignment | |||||||||||||||||||||
Location: | Bremen | |||||||||||||||||||||
Institutes and Institutions: | Institute of Space Systems > Systems Enabling Technologies | |||||||||||||||||||||
Deposited By: | Hüls, Simone | |||||||||||||||||||||
Deposited On: | 17 Mar 2016 10:12 | |||||||||||||||||||||
Last Modified: | 17 Mar 2016 10:12 |
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