A fuel-free spacecraft propelling system having an open-ended outer cylinder of a propelling device and an atomic oxygen collecting device is disclosed. The latter is arranged at the forwardly-propelled front end of the outer cylinder and is hermetically connected with an RF generating device and an ion cyclotron wave heating device through a magnetic confinement device. A spiral wave discharge oxygen plasma inlet and a spiral wave discharge oxygen plasma outlet in the ion cyclotron wave heating device are respectively provided with another magnetic confinement device. The propulsion of the invention does not need to carry the propellant, which greatly reduces the launch costs, enables a spacecraft to work on an orbit in the whole life circle work and is advantageous.


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    Titel :

    FUEL-FREE SPACECRAFT PROPELLING SYSTEM BASED ON SPATIAL ATOMIC OXYGEN


    Weitere Titelangaben:

    KRAFTSTOFFFREIES RAUMFAHRZEUGANTRIEBSSYSTEM AUF GRUNDLAGE VON IM WELTRAUM VORHANDENEN ATOMAREM SAUERSTOFF
    SYSTÈME DE PROPULSION DE VAISSEAU SPATIAL SANS CARBURANT BASÉ SUR L'OXYGÈNE ATOMIQUE SPATIAL


    Beteiligte:
    YI ZHONG (Autor:in) / ZHANG CHAO (Autor:in) / MENG LIFEI (Autor:in) / JIANG HAIFU (Autor:in) / LIU YENAN (Autor:in) / XIAO QI (Autor:in) / JIANG LIXIANG (Autor:in) / YU ZHAOJI (Autor:in)

    Erscheinungsdatum :

    2019-07-17


    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



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