A heat transfer control structure includes: an outer shell having an outer surface and an inner surface, the outer shell being heated by airflow along the outer surface; an inner shell disposed opposed to the inner surface of the outer shell, the inner shell being configured to accommodate a payload therein; and a plate coupled to the inner shell such that the plate is opposed to the inner shell across a gap. The outer shell is coupled to the plate.


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    Titel :

    Heat transfer control structure, flying object and spacecraft with high heat resistance


    Beteiligte:
    KATSUNAGA KENTA (Autor:in) / INAGAKI TADASHI (Autor:in)

    Erscheinungsdatum :

    26.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16L PIPES , Rohre



    HEAT TRANSFER CONTROL STRUCTURE, FLYING OBJECT AND SPACECRAFT WITH HIGH HEAT RESISTANCE

    KATSUNAGA KENTA / INAGAKI TADASHI | Europäisches Patentamt | 2021

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