Gemini vibration program includes ground tests on components, module, and whole vehicle to demonstrate launch withstanding capability of guidance, power, maneuvering, and environmental control systems; random vibration testing were conducted on three modules, namely fuel cell, short mission orbital attitude maneuvering system (OAMS), and long mission OAMS; excitation for tests was longitudinal and radial.


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    Titel :

    Vibration design approval and acceptance test program for Gemini spacecraft-component, module and whole vehicle testing


    Weitere Titelangaben:

    U S Naval Research Laboratory -- Shock Vibration Bul 35


    Beteiligte:
    Daiber, J.R. (Autor:in) / Noonan, V.S. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :