The electronic and other payload power densities in future micro/nano spacecraft are expected to exceed 25 Watts/cm(sup 2) and require advanced thermal control concepts and technologies to keep their payload within allowable temperature limits. This paper presents background on the need for pumped liquid cooling systems for future micro/nano spacecraft and results from this ongoing experimental investigation.


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    Titel :

    MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control


    Beteiligte:
    Birur, G. C. (Autor:in) / Shakkottai, P. (Autor:in) / Sur, T. W. (Autor:in)

    Kongress:

    NanoSpace 2001: Exploring Interdisciplinary Frontiers, International Conference


    Erscheinungsdatum :

    2000-11-20


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Micro/Nano spacecraft thermal control using MEMS based pumped liquid cooling systems

    Birur, G. C. / Shakkottai, P. / Green, A. et al. | NTRS | 2001


    Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system

    Birur, G. C. / Sur, T. W. / Paris, A. D. et al. | NTRS | 2001


    Micro/nano spacecraft thermal control using a MEMS-based pumped liquid cooling system

    Birur, G.C. / Waniewski Sur, T. / Paris, A.D. et al. | Tema Archiv | 2001


    Mechanical Pumped Cooling Loop for Spacecraft Thermal Control

    Birur, Gajanana C. / Gram, Marsh B. / Bhandari, Pradeep | SAE Technical Papers | 1996