An intake system for an atmosphere-breathing electric thruster is disclosed, comprising an inlet for inflow of atmosphere particles, an outlet for coupling to the thruster for fueling collected atmosphere particles to the thruster, a collector arranged between the inlet and the outlet comprising multiple channels for allowing inflowing atmosphere particles to pass through the channels towards the outlet, the channels defining an inlet area and a length, wherein a position of at least part of the channels is adjustable to alter at least one of the inlet area and the length.


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    Titel :

    INTAKE SYSTEM FOR AN ATMOSPHERE BREATHING ELECTRIC THRUSTER FOR A SPACECRAFT


    Beteiligte:
    QUANG DAMIEN LE (Autor:in) / ALSALIHI ZUHEYR (Autor:in) / PARODI PIETRO (Autor:in)

    Erscheinungsdatum :

    2021-08-26


    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



    INTAKE SYSTEM FOR AN ATMOSPHERE BREATHING ELECTRIC THRUSTER, SPACECRAFT

    QUANG DAMIEN LE / ALSALIHI ZUHEYR / PARODI PIETRO | Europäisches Patentamt | 2021

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    Intake system for an atmosphere breathing electric thruster for a spacecraft

    QUANG DAMIEN LE / ALSALIHI ZUHEYR / PARODI PIETRO | Europäisches Patentamt | 2024

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    INDUCTIVE PLASMA THRUSTER (IPT) DESIGN FOR AN ATMOSPHERE-BREATHING ELECTRIC PROPULSION SYSTEM (ABEP)

    Romano, Francesco / Herdrich, Georg / Roberts, Peter C. E | TIBKAT | 2020


    Intake design for an Atmosphere-Breathing Electric Propulsion System (ABEP)

    Romano, F. / Espinosa-Orozco, J. / Pfeiffer, M. et al. | Elsevier | 2021