A general approach to the structural design and verification used to determine the structural margins of the space vehicle elements under Marshall Space Flight Center (MSFC) management is described. The Space Shuttle results and organization will be used as illustrations for techniques discussed. Given also are: (1) the system analyses performed or to be performed by, and (2) element analyses performed by MSFC and its contractors. Analysis approaches and their verification will be addressed. The shuttle procedures are general in nature and apply to other than shuttle space vehicles.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Structural Margins Assessment Approach


    Beteiligte:
    R. S. Ryan (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    56 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Structural Margins Assessment Approach

    Ryan, Robert S. | NTRS | 1988


    Review and Assessment of JPL's Thermal Margins

    Siebes, G. / Kingery, C. / Farguson, C. et al. | British Library Conference Proceedings | 2012


    Review and Assessment of JPL's Thermal Margins

    Siebes, G. / Kingery, C. / Farguson, C. et al. | AIAA | 2012


    Thermal Margins for Flight Electronics Review and Assessment

    Siebes, G. / Kingery, C. / Farguson, C. et al. | NTRS | 2012


    Short margins

    Online Contents | 1994