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Contamination character of materials in space technology testing.Determination of the nature and degree of contamination of mirrors in a vacuum environment in the presence of UV irradiation by outgases from some materials that are candidates for use inside spacecraft and simulated spacecraft environments. A vacuum apparatus was developed for testing contamination of mirrors. Offgases from heated test materials are deposited on a refrigerated mirror, half of which is UV irradiated. Reflectance is measured between 1100 and 25,000 A. Thermofit RNF-100, insulated wire TRT-24-19-V-93, and Eccofoam FS and FPH gave heavier deposits on the nonirradiated mirror. Moxness MS60 SO8, Scotch Tape Y-9050, RTV-577, RTV-41, Stycast 1090, and Epon 934 and 828 gave heavier deposits on the irradiated mirror. Raychem wire 44/0411, polyimide tape X1156, Insulgrease G-640, High Vacuum Silicone Grease, and RTV-602 gave only slight deposits on the irradiated and nonirradiated areas of the mirror.
Document ID
19720041542
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coulson, D. M.
Haynes, D. L.
(Stanford Research Institute Menlo Park, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
AIAA PAPER 72-267
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: San Antonio, TX
Start Date: April 10, 1972
End Date: April 12, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A25208
Funding Number(s)
CONTRACT_GRANT: NAS5-11697
Distribution Limits
Public
Copyright
Other

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