An electrospray thruster includes an emitter including an array of tips, each tip of the array of tips being configured to emit ionic liquid, and an extractor electrode spaced from the emitter and comprising a conductive film, the conductive film having a plurality of apertures, the plurality of apertures being aligned with the array of tips of the emitter. The conductive film has a thickness such that an electrical short between the extractor electrode and the ionic fluid emitted from a respective tip of the array of tips ablates a portion of the conductive film along the aperture of the plurality of apertures aligned with the respective tip of the array of tips


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    Titel :

    ELECTROSPRAY THRUSTER SELF-PRESERVATION


    Weitere Titelangaben:

    SELBSTKONSERVIERUNG EINES ELEKTROSPRAY-TRIEBWERKS
    AUTO-CONSERVATION DE PROPULSEUR PAR ÉLECTRONÉBULISATION


    Beteiligte:
    JORNS BENJAMIN (Autor:in) / WHITTAKER COLLIN B (Autor:in) / SODANO HENRY (Autor:in)

    Erscheinungsdatum :

    23.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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 / H05H Plasmatechnik , PLASMA TECHNIQUE



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