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Radiation Exposure of Selected Composites and Thin FilmsThe effect of electron radiation on selected candidate composite materials was investigated. Radiation damage mechanisms were identified and the coefficient of thermal expansion were measured for each type composite material. It was concluded that the threshold for major physical and mechanical property changes in the polysulfone films and in the polysulfone and epoxy composites is in excess of 1 x 10 to the 9th power rads of electrons. Based upon these data, the 5208 and 934 epoxies and the P1700 polysulfone composites would be acceptable for 5 to 10 year geosynchronous Earth environment missions receiving 1 x 10 to the 9th power rads of electron radiation.
Document ID
19810010645
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wayne S Slemp
(Langley Research Center Hampton, United States)
Beatrice Santos
(Langley Research Center Hampton, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Publication Information
Publication: Large Space Systems Technology, 1980, Volume 1
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Launch Vehicles And Space Vehicles
Meeting Information
Meeting: Second Annual Technical Review
Location: Hampton, VA
Country: US
Start Date: November 18, 1980
End Date: November 20, 1980
Sponsors: National Aeronautics and Space Administration
Accession Number
81N19172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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