The Capillary Pumped Loop Flight Experiment (CAPL) is a prototype of the Earth Observing System (EOS) instrument thermal control systems. Four CAPL flight hardware components were tested in the Instrument Thermal Test Bed at NASA's Goddard Space Flight Center. The components tested were the capillary cold plates, capillary starter pump, heat pipe heat exchangers (HPHXs), and reservoir. The testing verified that all components meet or exceed their individual performance specifications. Consequently, the components have been integrated into the CAPL experiment which will be flown on the Space Shuttle in late 1993.


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    Titel :

    Testing of Flight Components for the Capillary Pumped Loop Flight Experiment


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Butler, Dan (Autor:in) / Ku, Jentung (Autor:in) / Ottenstein, Laura (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1993



    Erscheinungsdatum :

    01.07.1993




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Testing of flight components for the capillary pumped loop flight experiment

    Ottenstein, L. / Ku, Jentung / Butler, D. | Tema Archiv | 1993


    Flight Testing of the Capillary Pumped Loop Flight Experiment

    Butler, Dan / Ku, Jentung / Ottenstein, Laura | SAE Technical Papers | 1995


    Flight Testing of the Capillary Pumped Loop Flight Experiment

    Butler, D. / Ottenstein, L. / Ku, J. et al. | British Library Conference Proceedings | 1995


    Flight Testing of the Capillary Pumped Loop Flight Experiment

    Butler, D. / Ottenstein, L. / Ku, J. et al. | British Library Conference Proceedings | 1995


    Flight Testing of the Capillary Pumped Loop 3 Experiment

    Ottenstein, L. / Butler, D. / Ku, J. et al. | British Library Conference Proceedings | 2003