An electromagnetic energy momentum thruster has a cavity resonator and an electromagnetic radiation source for emitting an electromagnetic wave in evanescence into the cavity resonator. The electromagnetic wave produces a greater electromagnetic field amplitude and a greater electromagnetic radiation pressure on a primary interior surface area of the cavity resonator than on a secondary interior surface area of the cavity resonator. The difference between the electromagnetic field amplitude on the primary interior surface area and on the secondary interior surface area of the cavity resonatorforms a highly directional electromagnetic energy momentum tensor and provides a highly directional general relativistic metric tensor. As a result, a force is produced on the cavity resonator in theform of a thrust or an acceleration that propels the device in a direction substantially perpendicular to the primary interior surface area.

    一种电磁能动量推进器具有空腔谐振器和用于将消散的电磁波发射到空腔谐振器中的电磁辐射源。电磁波在空腔谐振器的主要内表面区域上比在空腔谐振器的次要内表面区域上产生更大的电磁场振幅和更大的电磁辐射压力。空腔谐振器的主要内表面区域上的和次要内表面区域上的电磁场振幅之间的差形成高度定向的电磁能动量张量,并提供高度定向的一般相对论度量张量。结果,在空腔谐振器上产生推力或加速度形式的力,该力在基本上垂直于主要内表面区域的方向上推进该装置。


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    Titel :

    ELECTROMAGNETIC ENERGY MOMENTUM THRUSTER USING TAPERED CAVITY RESONATOR EVANESCENT MODES


    Weitere Titelangaben:

    使用锥形空腔谐振器消散模式的电磁能动量推进器


    Beteiligte:
    FLANAGAN KYLE B (Autor:in) / DOHM PETER C (Autor:in)

    Erscheinungsdatum :

    29.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    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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