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Study of outgassing and decomposition of space shuttle heat protection tiles, fillers and adhesiveThe purpose of this project was to determine the chemicals desorbing from the space shuttle heat protection tiles. The original protocol for this project involved direct insertion probe mass spectrometry (DIPMS) analysis of the outgassing products from the tiles. However, this method proved unsatisfactory due to the large number of compounds desorbing from the tiles. A purge and trap technique was then employed to collect and separate the chemicals desorbing from the tiles. The maximum temperature in this analysis was 180 C which is the gas chromatograph fused silica capillary column's temperature limit. The desorption was also carried out at atmospheric pressure with helium as the purge gas. A description of the modified protocol is given. All compounds are tentatively identified.
Document ID
19850012932
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Proctor, B. L.
(Texas Univ. Dallas, TX, United States)
Hoffman, J. H.
(Texas Univ. Dallas, TX, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1982
Subject Category
Space Transportation
Report/Patent Number
NAS 1.26:175565
NASA-CR-175565
Report Number: NAS 1.26:175565
Report Number: NASA-CR-175565
Accession Number
85N21242
Funding Number(s)
CONTRACT_GRANT: NAG1-256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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