A component assembly for a space environment includes a main body, and a plurality of main body openings in the main body. Each main body opening has an identical cross-sectional shape. A plurality of inserts are installed to the main body at respective main body openings of the plurality of main body openings. Each insert of the plurality of inserts defines a fluid port for a fluid flow to flow into the main body or out of the main body via the respective main body openings. At least two fluid ports have a different cross-sectional configuration.


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    Titel :

    ADJUSTABLE PORT SIZE INSERT


    Beteiligte:
    HIMMELMANN ASHLEY ROSE (Autor:in) / KAUFMAN CORY (Autor:in) / FRAZIER MIGUEL (Autor:in) / NAGPAL ARJUN (Autor:in)

    Erscheinungsdatum :

    02.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B04C APPARATUS USING FREE VORTEX FLOW, e.g. CYCLONES , Zentrifugalapparate mit freier Wirbelströmung, z.B. Zyklone



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