Spacecraft are subjected to a variety of dynamics environments, which may include: quasi-static, vibration and acoustic loads at launch: pyrotechnic shocks generated by separation mechanisms; on orbit jitter; and sometimes, planetary landing loads. There is a trend in the aerospace industry to rely more on structural analyses and less on testing to simulate these environments, because dynamics testing of spacecraft is time consuming, risky and expensive.


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    Title :

    Vibration and acoustic testing of spacecraft


    Contributors:

    Conference:

    International Congress of Sound and Vibration


    Publication date :

    2002-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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