The test specifications for spacecraft and components permit test levels to be reduced under a procedure commonly referred to as notching. A summary is provided of the steps required to comply with the notching criterion. Primary structural loads are discussed along with aspect of mathematical modelling of the spacecraft structure, a launch loads analysis, a vibration test loads analysis, and notching methods. It is shown that current, general vibration test specifications are capable of producing unrealistically high spacecraft structural loads.


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    Titel :

    Avoiding unrealistic overtest by notching the vibration test specification


    Beteiligte:

    Kongress:

    Annual Meeting on the Cost effectiveness in the environmental sciences ; 1974 ; Washington, DC


    Erscheinungsdatum :

    01.01.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Minuteman Stage I overtest results

    ANDERSON, G. | AIAA | 1976


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    Koiter, W.T. | Online Contents | 1996


    Tube notching method, and associated notching machine

    BAUDY SEBASTIEN | Europäisches Patentamt | 2015

    Freier Zugriff