NASA LogoNTRSNTRS - NASA Technical Reports ServerSearchmore_vertCollectionsAboutNewsHelpLogin Back to ResultsThe Erosion of Diamond and Highly Oriented Pyrolytic Graphite After 1.5 Years of Space ExposurePolymers and other oxidizable materials on the exterior of spacecraft in the low Earth orbit (LEO) space environment can be eroded due to reaction with atomic oxygen (AO). Therefore, in order to design durable spacecraft, it is important to know the LEO AO erosion yield (Ey, volume loss per incident oxygen atom) of materials susceptible to AO reaction. The Polymers Experiment was developed to determine the AO Ey of various polymers and other materials flown in ram and wake orientations in LEO. The experiment was flown as part of the Materials International Space Station Experiment 7 (MISSE 7) mission for 1.5 years on the exterior of the International Space Station (ISS). As part of the experiment, a sample containing Class 2A diamond (100 plane) and highly oriented pyrolytic graphite (HOPG, basal and edge planes) was exposed to ram AO and characterized for erosion. The materials were salt-sprayed prior to flight to provide isolated sites of AO protection. The Ey of the samples was determined through post-flight electron microscopy recession depth measurements. The experiment also included a Kapton H witness sample for AO fluence determination. This paper provides an overview of the MISSE 7 mission, a description of the flight experiment, the characterization techniques used, the mission AO fluence, and the LEO Ey results for diamond and HOPG (basal and edge planes). The data is compared to the Ey of pyrolytic graphite exposed to four years of space exposure as part of the MISSE 2 mission. The results indicate that diamond erodes, but with a very low Ey of 1.58 +/- 0.04 x 10(exp -26) cm(exp 3)/atom. The different HOPG planes displayed significantly different amounts of erosion from each other. The HOPG basal plane had an Ey of 1.05 +/- 0.08 x 10(exp -24) cm(exp 3)/atom while the edge plane had a lower Ey of only 5.38 +/- 0.90 x 10(exp -25) -cm(exp 3)/atom. The Ey data from this ISS spaceflight experiment provides valuable information for understanding of chemistry and chemical structure dependent modeling of AO erosion.Document ID20180001293Acquisition SourceGlenn Research CenterDocument TypeTechnical Memorandum (TM)AuthorsDe Groh, Kim K.*(NASA Glenn Research Center Cleveland, OH, United States)*Banks, Bruce A.*(Science Applications International Corp. (SAIC) Cleveland, OH, United States)*Date AcquiredFebruary 20, 2018Publication DateFebruary 1, 2018Subject CategorySpacecraft Design, Testing And PerformanceReport/Patent NumberNASA/TM-2018-219756GRC-E-DAA-TN51758E-19468Funding Number(s)CONTRACT_GRANT: NNC12BA01BWBS: WBS 291647.01.22Distribution LimitsPublicCopyrightPublic Use Permitted.KeywordserosionInternational Space StatioAtomic oxygenspaceflight experimentAvailable DownloadsNameType20180001293.pdfSTIcloud_downloadcontent_copyvisibilityRelated RecordsThere are no records associated with this record.visibility_offNo Preview Available
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