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.


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    Title :

    Materials Opportunity for Spacecraft and Aerospace Thermal Management


    Contributors:

    Conference:

    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)


    Published in:

    Publication date :

    2005-02-06


    Size :

    10 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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