Results of the ASTRO-1 preliminary design review coupled loads analysis are presented. The M6.0Y Generic Shuttle mathematical models were used. Internal accelerations, interface forces, relative displacements, and net e.g., accelerations were recovered for two ASTRO-1 payloads in a tandem configuration. Twenty-seven load cases were computed and summarized. Load exceedences were found and recommendations made.


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    Title :

    ASTRO-1 Preliminary Design Review Coupled Load Analysis


    Contributors:

    Publication date :

    1984


    Size :

    881 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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