DocumentCode
2347200
Title
Properties of high thermal conductivity carbon-carbon composites for thermal management applications
Author
Golecki, Ilan ; Xue, Liang ; Leung, Roger ; Walker, Terence ; Anderson, Alec ; Dewar, Douglas ; Duncan, Chris ; Van Horik, Jon
Author_Institution
Res. & Technol., Allied-Signal Inc., Morristown, NJ, USA
fYear
1998
fDate
22-27 Feb 1998
Firstpage
190
Lastpage
195
Abstract
Carbon (fiber)-carbon (matrix) composites have the highest thermal conductivity per unit density among materials suitable for thermal management applications. C-C composites also have high toughness and their mechanical strength increases with temperature. We have developed C-C materials and structures for heat management applications at elevated temperatures, using pitch-based fiber preforms. Densities of 2.0-2.2 g/cm3, in-plane thermal conductivity of 690 W/m.K and tensile strength of 400 MPa have been measured in thin panels. Structures suitable for thermal management aerospace applications have been fabricated
Keywords
aerospace instrumentation; carbon fibre reinforced composites; cooling; high-temperature electronics; tensile strength; thermal conductivity; thermal management (packaging); C; C-C composites; C-C materials; C-C structures; carbon fiber-carbon matrix composites; carbon-carbon composites; composite density; heat management applications; in-plane thermal conductivity; mechanical strength; pitch-based fiber preforms; tensile strength; thermal conductivity; thermal management; thermal management aerospace applications; thermal management applications; toughness; Aerospace materials; Composite materials; Conducting materials; Fabrics; Heat sinks; Organic materials; Preforms; Temperature; Thermal conductivity; Thermal management;
fLanguage
English
Publisher
ieee
Conference_Titel
High-Temperature Electronic Materials, Devices and Sensors Conference, 1998
Conference_Location
San Diego, CA
Print_ISBN
0-7803-4437-5
Type
conf
DOI
10.1109/HTEMDS.1998.730696
Filename
730696
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