A Neutralizer for an ion thruster of a spacecraft comprises a cathode for emission of electrons, a support with an opening inside which the cathode is supported in a radially spaced manner, and an electrically conductive shielding which surrounds said opening and is electrically insulated from the support, wherein a ring is mounted between the shielding and the cathode and is electrically insulated from the shielding and radially spaced from the cathode.


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    Titel :

    Neutralizer for an ion thruster of a spacecraft


    Beteiligte:
    KREJCI DAVID (Autor:in) / KOCH QUIRIN (Autor:in)

    Erscheinungsdatum :

    17.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    NEUTRALIZER FOR AN ION THRUSTER OF A SPACECRAFT

    KREJCI DAVID / KOCH QUIRIN | Europäisches Patentamt | 2023

    Freier Zugriff

    Characterization of an Ion Thruster Neutralizer

    Foster, John / Williams, George / Patterson, Michael | AIAA | 2005


    Characterization of an Ion Thruster Neutralizer

    John Foster / George Williams / Michael Patterson | AIAA | 2007


    Characterization of an Ion Thruster Neutralizer

    Foster, J.E. | Online Contents | 2007