The present invention relates to a momentum dump method of a satellite reaction wheel to which an offset is applied. The present invention is to provide a momentum dump method of a satellite reaction wheel to which an offset is applied, which enables safer and more efficient operation of a satellite by applying an appropriate offset to the originally designed momentum dump.

    본 발명은 오프셋을 적용한 인공위성 반작용휠의 모멘텀 덤프 방법에 관한 것이다. 본 발명의 목적은, 원래 설계된 모멘텀 덤프에 대하여 적절한 오프셋을 적용함으로써 인공위성을 보다 안전하고 효율적으로 운용할 수 있도록 하는, 오프셋을 적용한 인공위성 반작용휠의 모멘텀 덤프 방법을 제공함에 있다.


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    Titel :

    Offset applied momentum dump method for reaction wheel of satellite


    Weitere Titelangaben:

    오프셋을 적용한 인공위성 반작용휠의 모멘텀 덤프 방법


    Beteiligte:
    YOON HYUNGJOO (Autor:in) / PARK YOUNG WOONG (Autor:in)

    Erscheinungsdatum :

    2021-05-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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