Ground Vacuum Facility to Simulate Low Earth Orbit Plasma Environment

This paper presents a large vacuum facility (6-ft-diameter, 10-ft-long chamber) equipped with a magnetic filter-type low Earth orbit plasma source. A recommended operating envelope for the plasma source was established through single-point measurements by varying the discharge currents of the plasma source and the gas flow rates. A three-axis translation stage was fabricated and tested with 2D and 3D scans of the simulated plasma environment. The measured plasma density during this study was between [Formula: see text] for the electrons and [Formula: see text] for the ions, whereas the electron and ion temperatures ranged from 0.55 to 2.06 eV and 1 to 3 eV, respectively. The simulated plasma environment compares well with orbital equivalents, specifically the F layers of the ionosphere.

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Publication Details

Journal
Journal of Spacecraft and Rockets
Published
2024-09-01
DOI
https://doi.org/10.2514/1.a36013
Citations
2
Primary Topic
Ionosphere and magnetosphere dynamics
Type
article
Field-Weighted Citation Impact
0.66

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article

Ground Vacuum Facility to Simulate Low Earth Orbit Plasma Environment

Daoru Han, Emmanuel Kofi Asuako Wie-Addo, Jacob Ortega
2 citations
Journal of Spacecraft and Rockets
Ionosphere and magnetosphere dynamics
0.66
article

Ground Vacuum Facility to Simulate Low Earth Orbit Plasma Environment

Daoru Han, Emmanuel Kofi Asuako Wie-Addo, Jacob Ortega
article en
2 citations

Abstract

This paper presents a large vacuum facility (6-ft-diameter, 10-ft-long chamber) equipped with a magnetic filter-type low Earth orbit plasma source. A recommended operating envelope for the plasma source was established through single-point measurements by varying the discharge currents of the plasma source and the gas flow rates. A three-axis translation stage was fabricated and tested with 2D and 3D scans of the simulated plasma environment. The measured plasma density during this study was between [Formula: see text] for the electrons and [Formula: see text] for the ions, whereas the electron and ion temperatures ranged from 0.55 to 2.06 eV and 1 to 3 eV, respectively. The simulated plasma environment compares well with orbital equivalents, specifically the F layers of the ionosphere.

Journal of Spacecraft and RocketsVol. 61(5)
Missouri University of Science and Technology (US)
National Science Foundation, National Aeronautics and Space Administration, Air Force Office of Scientific Research
Openalex Percentile: Top 28%
Ionosphere and magnetosphere dynamics
0.66
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