Integration of a Stirling cycle cryocooler into a flight system will require careful attention to the thermal, structural, and electrical interfaces between the cryocooler, the instrument and the spacecraft. These issues are currently under investigation by National Aeronautics and Space Administration/Goddard Space Flight Center personnel in laboratory tests of representative longlife cryocoolers. An 80 K cryocooler has been instrumented as a testbed for vibration control systems characterization. Initial vibration data using a new six-DOF force dynamometer is presented in this report.


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    Titel :

    Structural and thermal interface characteristics of Stirling cycle cryocoolers for space applications


    Beteiligte:
    Boyle, R. (Autor:in) / James, E. (Autor:in) / Miller, P. (Autor:in) / Arillo, V. (Autor:in) / Sparr, L. (Autor:in) / Castles, S. (Autor:in)


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Numerical Modeling of Stirling Cryocoolers

    Bauwens, L. / AIAA | British Library Conference Proceedings | 1994


    Thermal Performance of Stirling-Cycle Cryocoolers: A Comparison of JPL-Tested Coolers

    Smedley, G. T. / Mon, G. R. / Johnson, D. L. et al. | NTRS | 1994