An apparatus and method for mitigating the shock front of a rocket or aerospace plane flying at hypersonic speeds while simultaneously distilling liquid chemical elements from the ambient air. The invention employs supercooling driven by the cryogenic power of liquid hydrogen and/or regenerative evaporation of liquid hydrogen and/or liquid nitrogen to drive isothermal compression and consequentially usurp the shock front in totality.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Superconductive Hypersonic Liquefaction Nosecone


    Beteiligte:
    JANEKE CHARL E (Autor:in)

    Erscheinungsdatum :

    28.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Superconductive hypersonic liquefaction nosecone

    JANEKE CHARL EMELIO | Europäisches Patentamt | 2015

    Freier Zugriff

    Apparatus and Methods for Hypersonic Nosecone

    JANEKE CHARL E | Europäisches Patentamt | 2015

    Freier Zugriff

    Apparatus and methods for hypersonic nosecone

    JANEKE CHARL E | Europäisches Patentamt | 2016

    Freier Zugriff

    Nosecone Design to Withstand Hypersonic Debris Impact

    Drenth, Aaron / Anderson, Michael L. | AIAA | 2025


    PLATED POLYMER NOSECONE

    ROACH JAMES T / KLING COLIN J / COOK GRANT O et al. | Europäisches Patentamt | 2016

    Freier Zugriff