The patent relates to a system for controlling the annular nozzle throat area (and hence the thrust) of a solid-propellant rocket by means of a pintle or plug the position of which is caused to vary in response to pressure variations within the combustion chamber of the rocket.


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    Titel :

    System for Controlling the Nozzle Throat Area of a Rocket Motor


    Beteiligte:
    J. D. Beardsley (Autor:in) / J. D. Shipley (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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