Space Shuttle users are required to design their payload to the Shuttle loads environment. This loads environment covers mission phases from prelaunch to landing. Transient response loads analyses are required for lift-off and landing events. Other mission events are analyzed statically because they result in payload loads that either change slowly or are lower than lift-off and landing loads. Response data from flight instrumentation located on the orbiter and payloads have been compared to preflight design conditions and to nominal predictions. The results have verified that the design loads envelop flight responses.


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    Titel :

    Loads environment for payload/cargo integration


    Beteiligte:
    Frederick, D. H. (Autor:in) / Haugen, E. A. (Autor:in) / Hamilton, D. A. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1983 ; Reno, NV


    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Loads environment for payload/cargo integration

    FREDERICK, D. / HAUGEN, E. / HAMILTON, D. | AIAA | 1983





    Improvements to Payload/Cargo Leakage Verification

    Lvovsky, O. / Grayson, C. / International Association for the Advancement of Space Safety; European Space Agency | British Library Conference Proceedings | 2009