This paper details the flight configuration and pre-flight performance test results of the fifth generation cryogenic capillary pumped loop (CCPL-5). This device will fly on STS-95 in October 1998 as part of the CRYOTSU Flight Experiment. This flight represents the first in-space demonstration of a CCPL; a miniaturized two-phase fluid circulator for thermally linking cryogenic components. CCPL-5 utilizes N2 as the working fluid and has a practical operating range of 75-110 K. Test results indicate that CCPL-5, which weighs about 200 grams, can transport over 10 W of cooling a distance of 0.25 m (or more) with less than a 5 K temperature drop.


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    Titel :

    Design and Testing of a Cryogenic Capillary Pumped Loop Flight Experiment


    Beteiligte:
    Bugby, David C. (Autor:in) / Kroliczek, Edward J. (Autor:in) / Ku, Jentung (Autor:in) / Swanson, Ted (Autor:in) / Tomlinson, B. J. (Autor:in) / Davis, Thomas M. (Autor:in) / Baumann, Jane (Autor:in) / Cullimore, Brent (Autor:in)

    Erscheinungsdatum :

    01.11.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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