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Atomic Oxygen Erosion Yield Predictive Tool for Spacecraft Polymers in Low Earth OrbitA predictive tool was developed to estimate the low Earth orbit (LEO) atomic oxygen erosion yield of polymers based on the results of the Polymer Erosion and Contamination Experiment (PEACE) Polymers experiment flown as part of the Materials International Space Station Experiment 2 (MISSE 2). The MISSE 2 PEACE experiment accurately measured the erosion yield of a wide variety of polymers and pyrolytic graphite. The 40 different materials tested were selected specifically to represent a variety of polymers used in space as well as a wide variety of polymer chemical structures. The resulting erosion yield data was used to develop a predictive tool which utilizes chemical structure and physical properties of polymers that can be measured in ground laboratory testing to predict the in-space atomic oxygen erosion yield of a polymer. The properties include chemical structure, bonding information, density and ash content. The resulting predictive tool has a correlation coefficient of 0.914 when compared with actual MISSE 2 space data for 38 polymers and pyrolytic graphite. The intent of the predictive tool is to be able to make estimates of atomic oxygen erosion yields for new polymers without requiring expensive and time consumptive in-space testing.
Document ID
20090011780
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Bank, Bruce A.
(Alphaport, Inc. Cleveland, OH, United States)
de Groh, Kim K.
(NASA Glenn Research Center Cleveland, OH, United States)
Backus, Jane A.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
August 24, 2013
Publication Date
December 1, 2008
Subject Category
Inorganic, Organic And Physical Chemistry
Report/Patent Number
E-16694
NASA/TM-2008-215490
Distribution Limits
Public
Copyright
Public Use Permitted.
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