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Active cleaning technique for removing contamination from optical surfaces in spacePlasma cleaning experiments were completed on hydrocarbon contaminant films, experiments were initiated to determine a satisfactory technique for depositing contaminant films, and an experiment was conducted to determine whether specimens are being thermally cleaned rather than plasma cleaned. Results of plasma cleaning experiments on hydrocarbon contaminant films showed that the optical properties of mirrors and gratings could be satisfactorily restored. Results on fused silica optical flats were inconclusive because of the insensitivity of measurement techniques to the contaminant films. White thermal control surfaces, degraded by the hydrocarbon contaminant film, could not be restored by oxygen plasma exposure. The reflectance of silvered FEP Teflon thermal control surfaces could be restored by plasma cleaning. Experiments with a silicone contaminant indicated that it could not be easily polymerized onto surfaces with ultraviolet radiation. Results of the thermal cleaning experiment showed that the polymerized hydrocarbon contaminant film could not be removed by heating in vacuum to a temperature in excess of that expected during plasma cleaning.
Document ID
19720005239
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gillette, R. B.
(Boeing Co. Seattle, WA, United States)
Beverly, W. D.
(Boeing Co. Seattle, WA, United States)
Date Acquired
August 6, 2013
Publication Date
November 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-121040
QPR-3
Report Number: NASA-CR-121040
Report Number: QPR-3
Accession Number
72N12888
Funding Number(s)
CONTRACT_GRANT: NAS8-26385
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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