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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    Title :

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


    Additional title:

    U S Naval Research Laboratory -- Shock Vibration Bul 35


    Contributors:
    Daiber, J.R. (author) / Noonan, V.S. (author)


    Publication date :

    1966


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :