A study was performed to determine venting design criteria for space shuttle payloads using worst case ascent, payload bay pressure profiles. This study incorporated the analytical model from an earlier study by Mironer and Regan, along with a number of worst case ascent pressure profiles provided by NASA/JSC. For each pressure profile, the resulting differential pressures were determined for a number of vent geometries. The maximum differential pressures for each profile were then plotted and overlayed as a function of the vent geometry. The results are summarized as a single curve that indicates the maximum differential pressure which can be expected for a given vent geometry. This curve should serve as a guideline for used in payload venting design.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Payload venting in worst case shuttle environments


    Weitere Titelangaben:

    Nutzlastoeffnungen bei schlechtesten Bedingungen fuer die Raumfaehre


    Beteiligte:
    Murri, B.W. (Autor:in)

    Erschienen in:

    AIAA-Papers ; Jun ; 1-3


    Erscheinungsdatum :

    1987


    Format / Umfang :

    3 Seiten, 4 Bilder, 1 Tabelle, 3 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






    Venting of Space-Shuttle payloads

    MIRONER, A. / REGAN, F. | AIAA | 1983


    Space shuttle compartment venting Final report

    Haukohl, J. / Robertson, S. J. | NTRS | 1971


    Space shuttle orbiter venting: Lessons learned

    Lutfi, H. S. / Nieder, R. L. | NTRS | 1983