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Applications of high thermal conductivity composites to electronics and spacecraft thermal designRecently, high thermal conductivity graphite fiber-reinforced metal matrix composites (MMCs) have become available that can save weight over present methods of heat conduction. Another significant advantage is that these materials can be used without the plumbing and testing complexities that accompany the use of liquid heat pipes. A spinoff of this research was the development of other MMCs as electronic device heat sinks. These use particulates rather than fibers and are formulated to match the coefficient of thermal expansion of electronic substrates in order to alleviate thermally induced stresses. The development of both types of these materials as viable weight-saving substitutes for the traditional methods of thermal control for electronics packaging and also for spacecraft thermal control applications are the subjects of this report.
Document ID
19900038554
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sharp, G. Richard
(NASA Lewis Research Center Cleveland, OH, United States)
Loftin, Timothy A.
(DWA Composite Specialties, Inc. Chatsworth, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
AIAA PAPER 90-0783
Meeting Information
Meeting: AIAA International Communication Satellite Systems Conference and Exhibit
Location: Los Angeles, CA
Country: United States
Start Date: March 11, 1990
End Date: March 15, 1990
Accession Number
90A25609
Distribution Limits
Public
Copyright
Other

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