Along with initial program, analysis must be made of entire vehicle design requirements to establish components and environments; reliability goals and allocations of subsystem goals; to illustrate technique for estimating reliability, preliminary estimate for proposed spacecraft power supply subsystem is presented; reliability emphasis in design study using statistical methods to devise economical configuration of redundant design; design review method; reliability during development; subsystem qualification testing.


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    Titel :

    Reliable spacecraft designs


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Doshay, I. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Design



    Erscheinungsdatum :

    1961


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reliable Spacecraft Designs

    Doshay, I. | SAE Technical Papers | 1961


    Lunar spacecraft designs

    Arthur, G.R. | Engineering Index Backfile | 1961


    Reliable software for spacecraft

    Hecht, H. | Tema Archiv | 1980


    Galileo Spacecraft Thermal Designs

    Kerry T. Nock | AIAA | 1991


    Making Reliable and Dependable Spacecraft

    Chechile, Ignacio | Springer Verlag | 2023