Vibration testing of spacecraft to levels of booster interface spectrum while supported by "rigid" fixtures is deemed unrealistic in that structural failures may be induced which would not occur on more compliant support of booster; limiting of shaker input forces at vehicle support points to design limit loads precludes this type of failure; random vibration tests conducted on P RIME SV-5D lifting body utilized this force limiting approach and techniques employed are described.


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    Titel :

    Flight level vibration testing of lifting body reentry vehicle


    Weitere Titelangaben:

    U S Naval Research Laboratory -- Shock and Vibration Bul


    Beteiligte:
    McCaa, R. (Autor:in) / Matrullo, M. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Lifting-body reentry vehicle

    Stadler, R. | AIAA | 1993


    Lifting-Body Reentry Vehicle

    Stadler, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1993




    Reentry vehicle flight testing and recovery techniques

    RIGALI, D. / STERK, M. / RANDMAA, J. | AIAA | 1980