Carbon‐carbon and polymer matrix composite materials for thermal panels are used in spacecrafts and planned for thermal management in high volume, aircraft electronics and power systems. The requirements are lightweight, highly performance conductive materials that can withstand the stresses in the specific applications. This evaluation investigates a number of emerging carbon‐carbon composites and baseline polymer matrix composite panels to evaluate their potential for thermal transfer applications. Properties were measured from −250 °F to +250 °F for generic space orbital applications.
Materials Opportunity for Spacecraft and Aerospace Thermal Management
SPACE TECHNOLOGY AND APPLICATIONS INT.FORUM-STAIF 2005: Conf.Thermophys in Micrograv;Conf Comm/Civil Next Gen.Space Transp; 22nd Symp Space Nucl.Powr Propuls.;Conf.Human/Robotic Techn.Nat'l Vision Space Expl.; 3rd Symp Space Colon.; 2nd Symp.New Frontiers ; 2005 ; Albuquerque, New Mexico (USA)
AIP Conference Proceedings ; 746 , 1 ; 22-31
2005-02-06
10 pages
Conference paper
Electronic Resource
English
Materials Opportunity for Spacecraft and Aerospace Thermal Management
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