The nozzle has a variable throat area for use with a rocket or other jet type motor. The nozzle employs a plurality of radially reciprocable probes for insertion into the nozzle throat to restrict the unobstructed area of the throat orifice.


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    Titel :

    Variable Throat Nozzle


    Beteiligte:
    S. L. Hardy (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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