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Modeling International Space Station (ISS) Floating PotentialsThe floating potential of the International Space Station (ISS) as a function of the electron current collection of its high voltage solar array panels is derived analytically. Based on Floating Potential Probe (FPP) measurements of the ISS potential and ambient plasma characteristics, it is shown that the ISS floating potential is a strong function of the electron temperature of the surrounding plasma. While the ISS floating potential has so far not attained the pre-flight predicted highly negative values, it is shown that for future mission builds, ISS must continue to provide two-fault tolerant arc-hazard protection for astronauts on EVA.
Document ID
20030003735
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ferguson, Dale C.
(NASA Glenn Research Center Cleveland, OH United States)
Gardner, Barbara
(Science Applications International Corp. San Diego, CA United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2002
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
NASA/TM-2002-211487
NAS 1.15:211487
AIAA Paper 2002-0933
Report Number: NASA/TM-2002-211487
Report Number: NAS 1.15:211487
Report Number: AIAA Paper 2002-0933
Meeting Information
Meeting: 40th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 14, 2002
End Date: January 17, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 755-A4-05
Distribution Limits
Public
Copyright
Public Use Permitted.
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