Consideration has been given to utilizing the external area of the Space Station common modules or resource nodes to provide heat rejection. A program was undertaken to define the best body mounted radiator design, to define and build a full size test article and to conduct testing to verify performance.Trade studies were conducted and a preferred design selected. The selected design employed high performance grooved heat pipes of an off-the-shelf design. Twenty panels, each about 1.2 m wide by 5.6 m long are installed on each module rejecting a total of about 12 kW. The radiators are interfaced with the module thermal control loop by use of a refrigerant 21 loop with an on-orbit operable disconnect at each panel. A one-panel test article has been designed and is currently being fabricated. Testing is scheduled to be conducted in June of 1987.


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    Titel :

    Space Station Body Mounted Radiator Design


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Fleming, M. L. (Autor:in) / Duschatko, R. J. (Autor:in)

    Kongress:

    Intersociety Conference on Environmental Systems ; 1987



    Erscheinungsdatum :

    1987-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Space station body mounted radiator design

    Fleming, M.L. / Duschatko, R.J. | Tema Archiv | 1987



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