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, and enables a spacecraft to advantageously have an increased orbit life over existing spacecraft systems.


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    Titel :

    Fuel-free spacecraft propelling system based on spatial atomic oxygen and propelling method


    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 :

    2017-10-24


    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



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