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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    Title :

    Reliable spacecraft designs


    Additional title:

    SAE -- Paper


    Contributors:
    Doshay, I. (author)

    Conference:

    SAE Meeting ; 1961 Design



    Publication date :

    1961


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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