The nozzle is for use with a rocket or other jet type motor. Cams are employed to shift the nozzle venturi axially with respect to a fixed conical probe projecting through it to thereby change the size of the unobstructed area of the throat orifice.


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    Titel :

    Variable Throat Nozzle


    Beteiligte:
    W. B. Wilson (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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