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Ultra-Lightweight Nanocomposite Foams and Sandwich Structures for Space Structure ApplicationsMicrocellular nanocomposite foams and sandwich structures have been created to have excellent electrical conductivity and radiation-resistant properties using a new method that does not involve or release any toxicity. The nanocomposite structures have been scaled up in size to 12 X 12 in. (30 X 30 cm) for components fabrication. These sandwich materials were fabricated mainly from PE, CNF, and carbon fibers. Test results indicate that they have very good compression and compression-after-impact properties, excellent electrical conductivity, and superior space environment durability. Compression tests show that 1000 ESH (equivalent Sun hours) of UV exposure has no effect on the structural properties of the sandwich structures. The structures are considerably lighter than aluminum alloy (= 36 percent lighter), which translates to 36 percent weight savings of the electronic enclosure and its housing. The good mechanical properties of the materials may enable the electronic housing to be fabricated with a thinner structure that further reduces the weight. There was no difficulty in machining the sandwich specimens into electronic enclosure housing.
Document ID
20120010463
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Tan, Seng
(Wright Materials Research Co. Beavercreek, OH, United States)
Date Acquired
August 26, 2013
Publication Date
June 1, 2012
Publication Information
Publication: NASA Tech Briefs, June 2012
Subject Category
Composite Materials
Report/Patent Number
MFS-32922-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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