The Combustion Module-2 (CM-2) is a space experiment that launches on Shuttle mission STS-107 in the SPACEHAB Double Research Module. The CM-2 flight hardware is installed into SPACEHAB single and double racks. The CM-2 flight hardware was vibration tested in the launch configuration to characterize the structure's modal response. Cross-orthogonality between test and analysis mode shapes were used to assess model correlation. Lessons learned for pre-test planning and model verification are discussed.


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    Titel :

    Lessons Learned From CM-2 Modal Testing and Analysis


    Beteiligte:

    Kongress:

    Ninth International Congress on Sound and Vibration ; 2002 ; Orlando, FL, United States


    Erscheinungsdatum :

    2002-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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