Applications of high thermal conductivity graphite fibers to space structures are discussed in the context of a composite scan mirror and composite battery sleeves. Both structures have competing thermal and structural requirements. The scan mirror design uses the high thermal conductivity graphite to reduce temperature gradients and thereby reduce thermal distortion. The battery sleeves achieve a significant mass savings by using the fiber to replace an aluminum part.


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    Titel :

    High thermal conductivity graphite in space applications


    Weitere Titelangaben:

    Graphit mit hoher Wärmeleitfähigkeit in Raumfahrtanwendugen


    Beteiligte:
    Peck, S.O. (Autor:in)


    Erscheinungsdatum :

    1995


    Format / Umfang :

    8 Seiten, 5 Bilder, 3 Tabellen, 3 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    High Thermal Conductivity Graphite in Space Applications

    Peck, S. / American Institute of Aeronautics and Astronautics| ASME| ASCE | British Library Conference Proceedings | 1995



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    Applications for High Thermal Conductivity Graphite Heat Sinks for Fighter Avionics

    Watts, Roland / Newland, Scott | SAE Technical Papers | 2004