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ISS Plasma Interaction: Measurements and ModelingIonospheric plasma interaction effects on the International Space Station are discussed in the following paper. The large structure and high voltage arrays of the ISS represent a complex system interacting with LEO plasma. Discharge current measurements made by the Plasma Contactor Units and potential measurements made by the Floating Potential Probe delineate charging and magnetic induction effects on the ISS. Based on theoretical and physical understanding of the interaction phenomena, a model of ISS plasma interaction has been developed. The model includes magnetic induction effects, interaction of the high voltage solar arrays with ionospheric plasma, and accounts for other conductive areas on the ISS. Based on these phenomena, the Plasma Interaction Model has been developed. Limited verification of the model has been performed by comparison of Floating Potential Probe measurement data to simulations. The ISS plasma interaction model will be further tested and verified as measurements from the Floating Potential Measurement Unit become available, and construction of the ISS continues.
Document ID
20040111048
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Barsamian, H.
(Boeing Co. Houston, TX, United States)
Mikatarian, R.
(Boeing Co. Houston, TX, United States)
Alred, J.
(Boeing Co. Houston, TX, United States)
Minow, J.
(Jacobs Sverdrup Technology, Inc. United States)
Koontz, S.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2004
Publication Information
Publication: 8th Spacecraft Charging Technology Conference
Subject Category
Plasma Physics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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