In one embodiment, an air-scoop includes an air inlet that air molecules enter the air-scoop through at an orbital speed when the air-scoop is moving through an atmosphere at the orbital speed. The air-scoop also includes a rotor that is rotated by a motor at a rotational speed, and the rotor includes multiple rotatable blade stages. A first one of the rotatable blade stages has a blade configuration that maximizes transparency of the first one of the rotatable blade stages to air molecules entering the air-scoop through the air inlet at the orbital speed when the rotor is rotating at the rotational speed. A last one of the rotatable blade stages has a blade configuration that maximizes opacity of the last one of the rotatable blade stages to air molecules in the air-scoop flowing directionally toward the air inlet when the rotor is rotating at the rotational speed.


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    Titel :

    TURBOMOLECULAR AIR-SCOOP FOR SATELLITE AIR-BREATHING ELECTRIC PROPULSION


    Weitere Titelangaben:

    TURBOMOLEKULARES LUFTGERÜST FÜR ELEKTRISCHEN ANTRIEB DURCH LUFTATMEN VON SATELLITEN
    BUSE D'ADMISSION D'AIR TURBOMOLÉCULAIRE POUR PROPULSION ÉLECTRIQUE AÉRIENNE PAR SATELLITE


    Beteiligte:

    Erscheinungsdatum :

    28.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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