Eighteen missiles of various configurations have been flight tested, and all of the components and systems have performed correctly. The major accomplishments of this program have been: 1) the proven capability of the design team to develop and flight test a complete fluidic control system in a reasonable schedule and for a reasonable cost, and 2) the proven repeatability, reliability, and ruggedness of the fluidics components during the experimental programs.


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    Titel :

    Fluidics in missile control systems


    Weitere Titelangaben:

    Fluidik in Flugkoerper-Regelungssystemen


    Beteiligte:
    Griffith, W.A. (Autor:in)

    Erschienen in:

    Fluidics Quarterly ; 6 , 3 ; 31-42


    Erscheinungsdatum :

    1974


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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