Feasibility of utilizing nozzle separation as method of thrust vector control is discussed; preceding work was mainly study and analysis of nozzle separation; these results are applied to guidance problem; possibility of using nozzle separation as method for thrust vector control is dealt with; guidance problem is reviewed and trend toward purely aerodynamic vectoring through secondary injection is discussed; nozzle separation approach is broken into two areas -- controllability and magnitude; tests in these areas indicate that nozzle separation can be controlled and is of adequate magnitude to complement secondary injection as means of thrust vectoring. (22915)


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    Titel :

    Controlled nozzle separation for thrust vectoring


    Weitere Titelangaben:

    AIAA Student J


    Beteiligte:
    Chasteen, L.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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