A miniature satellite that uses a modified structural frame in order to store and disperse propulsion fuel efficiently. The modified structural frame includes a plurality of structural members. Each of the plurality of structural members includes a tubular body, a first endcap, a second endcap, an outlet port, and an inlet port. The first endcap and the second endcap are oppositely positioned within the tubular body. The first endcap and the second endcap are each perimetrically connected to the tubular body in order to delineate a fuel storage volume. The inlet port is positioned in between the first endcap and the second endcap and is mechanically integrated into the tubular body. The outlet port disperses propulsion fuel and is also mechanically integrated into the tubular body. The inlet port is in fluid communication with the outlet port through the tubular body. Additionally, the structural members are mounted amongst each other.


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    Titel :

    Modified structural frame for storing propulsion fuel in a CubeSat


    Beteiligte:

    Erscheinungsdatum :

    30.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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