Choice and preliminary sizing of liquid injection Thrust Vector Control TVC system can be evaluated in early design stages of vehicle system; best point of fluid injection usually occurs about 1/3 of distance from throat of nozzle to end of expansion cone; liquid or gas injection will have less weight penalty to rocket only when total burning of rocket stage is less than 60 sec; to get best reliability factor for system, it should have capability of operating in presence of contamination; basic injector valve design and performance is controlled by maximum mass flow rate, slew response, frequency response, and hysteresis; block diagram.


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    Titel :

    Practical design of fluid injection thrust vector control systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Salemka, R.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Control



    Erscheinungsdatum :

    1964


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Liquid-Injection Thrust Vector Control.

    Richard J. Zeamer | AIAA | 1977


    Liquid injection thrust vector control

    Green, C.J. / McCullough, Jr., F. | Engineering Index Backfile | 1963