A magnetic nozzle having a converging/diverging contour shape that converts the thermal energy of a propellant into directed kinetic energy, but uses magnetic fields instead of a physical boundary to direct the flow of particles.


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    Title :

    Converging/diverging magnetic nozzle


    Contributors:

    Publication date :

    2022-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen



    Converging/diverging magnetic nozzle

    LONGMIER BENJAMIN / SHEEHAN JOHN PATRICK | European Patent Office | 2016

    Free access

    CONVERGING/DIVERGING MAGNETIC NOZZLE

    LONGMIER BENJAMIN / SHEEHAN JOHN PATRICK | European Patent Office | 2016

    Free access

    CONVERGING/DIVERGING MAGNETIC NOZZLE

    LONGMIER BENJAMIN / SHEEHAN JOHN PATRICK | European Patent Office | 2017

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    Mass transport in a converging-diverging nozzle

    Bauer, Helmut F. | TIBKAT | 1986


    Jet-Fuel Cavitation in a Converging-Diverging Nozzle

    Davis, Michael / Dunn, Patrick / Thomas, Flint | AIAA | 2007