Light weight, highly thermally conductive composites for space radiators

Jyh Ming Ting, Jason R. Guth, Max L. Lake

研究成果: Conference article同行評審

6 引文 斯高帕斯(Scopus)

摘要

Future power generation and consequent waste heat in space platforms will require innovative thermal management techniques in order to avoid overheating critical components. Potential candidates are composite materials with light weight and high thermal conductivity. Using the highest thermal conductivity fiber, i.e. vapor-grown carbon fiber, as reinforcement, we have developed polymer matrix composites useful for space radiators. These composite materials were characterized for thermal conductivity, coefficient of thermal expansion, and tensile strength and modulus. Microstructural analysis was also performed using optical and scanning electron microscopy.

原文English
頁(從 - 到)279-288
頁數10
期刊Ceramic Engineering and Science Proceedings
16
發行號4
出版狀態Published - 1995 七月 1
事件Proceedings of the 19th Annual Conference and Exhibition on Composites, Advanced Ceramics, Materials, and Structures-B. Part B - Cocoa Beach, FL, USA
持續時間: 1995 一月 81995 一月 12

All Science Journal Classification (ASJC) codes

  • 陶瓷和複合材料
  • 材料化學

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