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Atomic Oxygen Erosion of EVA-Stranded Soft-Goods on the ISSThis paper presents the results of an analysis to calculate the cumulative, effective atomic oxygen (AO) flux impinging on short-duration EVA tethers used to secure panel NOD1/C2-02 and panel LAB/C2-03. Shadowing from the ram reduces the AO flux on much of the Node 1 panel. On the Lab panel, the tethers are essentially in the ram flux. Table 1 summarizes the results of the analysis for Node 1 and the US Lab panels.
Document ID
20170004713
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Alred, John W. (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
May 24, 2017
Publication Date
May 15, 2017
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-39568-1
Report Number: JSC-CN-39568-1
Meeting Information
Meeting: The Applied Space Environments Conference 2017 (ICES 2017)
Location: Huntsville, AL
Country: United States
Start Date: May 15, 2017
End Date: May 19, 2017
Sponsors: Universities Space Research Association
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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