The Cryogenic Heat Pipe (CRYOHP) Experiment has been designed to test two cryogenic heat pipes independently in a micro-gravity environment. The CRYOHP experiment is manifested for flight aboard the shuttle (STS-53) which is scheduled for launch in November, 1992. This paper presents the design of this experiment and the thermal vacuum verification test results. A correlation of the test data and the planned mission operations are also provided.


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    Titel :

    Performance of the Cryogenic Heat Pipe Experiment


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Conference On Environmental Systems ; 1992



    Erscheinungsdatum :

    1992-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Performance of the Cryogenic Heat Pipe Experiment

    Brennan, Patrick J. / Stouffer, Charles / Thienel, Lee et al. | NTRS | 1992


    Cryogenic heat pipe experiment - Flight performance onboard a sounding rocket

    HARWELL, W. / QUADRINI, J. / SHERMAN, A. et al. | AIAA | 1975


    Design and performance of a Cryogenic Heat Pipe Experiment (CRYOHP)

    BEAM, JERRY / BRENNAN, PATRICK / BELLO, MEL | AIAA | 1992



    Flight data for the Cryogenic Heat Pipe (CRYOHP) Experiment

    BRENNAN, PATRICK / THIENEL, LEE / SWANSON, TED et al. | AIAA | 1993