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:
    M. E. McNelis (Autor:in) / T. W. Goodnight (Autor:in) / K. S. Carney (Autor:in) / K. D. Otten (Autor:in)

    Erscheinungsdatum :

    2002


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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