In ground testing prior to launch the static loads portion of the launch profile may be simulated by either applying static loads directly to the spacecraft through an appropriate loading facility or by subjecting the spacecraft to acceleration loads on a centrifuge. The factors to be considered in selecting one of the two simulation methods are discussed, giving attention to the relative advantages of the two methods in each case.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Selection of appropriate test method for simulating steady-state spacecraft launch loads


    Beteiligte:
    Shockey, E. F. (Autor:in) / Arcilesi, C. J. (Autor:in)

    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




    Spacecraft Launch Depressurization Loads

    Sanz-Andrés, Á | Online Contents | 1997


    Spacecraft Launch Depressurization Loads

    s, Juli-Uuml / n Santiago-Prowald / Antonio Ayuso-Barea | AIAA | 1997



    A simpler approach to update spacecraft launch loads

    AGRAWAL, B. / GROSSERODE, P. / HARCROW, H. et al. | AIAA | 1985