Space shuttle design verification requires dynamic data from full scale structural component and assembly tests. Wind tunnel and other scaled model tests are also required early in the development program to support the analytical models used in design verification. Presented is a design philosophy based on mathematical modeling of the structural system strongly supported by a comprehensive test program; some of the types of required tests are outlined.


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    Titel :

    Dynamic testing for shuttle design verification


    Beteiligte:
    Green, C. E. (Autor:in) / Leadbetter, S. A. (Autor:in) / Rheinfurth, M. H. (Autor:in)


    Erscheinungsdatum :

    01.07.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Dynamic analysis for shuttle design verification

    Fralich, R. W. / Green, C. E. / Rheinfurth, M. H. | NTRS | 1972


    Design verification testing of space shuttle main engine transducers

    Shedlov, M.W. / Myhre, D. | Tema Archiv | 1978