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Measurement of Thermal Properties of Composite Panels

[+] Author Affiliations
A. M. Druma, M. K. Alam

Ohio University, Athens, OH

M. Kistner, Roland Watts

AFRL/MLSC, Wright-Patterson AFB, OH

Paper No. HT-FED2004-56566, pp. 385-388; 4 pages
doi:10.1115/HT-FED2004-56566
From:
  • ASME 2004 Heat Transfer/Fluids Engineering Summer Conference
  • Volume 1
  • Charlotte, North Carolina, USA, July 11–15, 2004
  • Conference Sponsors: Heat Transfer Division and Fluids Engineering Division
  • ISBN: 0-7918-4690-3 | eISBN: 0-7918-3740-8
  • Copyright © 2004 by ASME

abstract

Thermal panels are used in spacecrafts and planned for thermal management in aircraft electronics and power systems. The requirements are light-weight, highly conductive emerging carbon materials that can withstand the stresses in the specific applications. A number of carbon fiber reinforced carbon-carbon and organic matrix composite panels were fabricated and tested by using a cryogenic Flash Diffusivity instrument and Differential Scanning Calorimeter (DSC). The properties were measured at cryogenic and above ambient temperatures.

Copyright © 2004 by ASME

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