A preliminary design analysis of a stand alone payload integration device (IVE) is provided that is capable of verifying payload compatibility in form, fit and function with the shuttle orbiter prior to on-line payload/orbiter operations. The IVE is a high fidelity replica of the orbiter payload accommodations capable of supporting payload functional checkout and mission simulation. A top level payload integration analysis developed detailed functional flow block diagrams of the payload integration process for the broad spectrum of P/L's and identified degree of orbiter data required by the payload user and potential applications of the IVE.


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    Titel :

    Shuttle payload interface verification equipment study. Volume 1: Executive summary


    Erscheinungsdatum :

    1976-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch