The invention relates to a glass panel for an aircraft suitable for a suborbital flight and an aeronautical flight. The glass panel comprises an outer panel (1) made of polycarbonate or aluminosilicate for temperature resistance, a main panel (2) for pressure resistance, sized according to standard aeroplane safety factors, and an inner panel (3), providing redundancy for the main panel, sized with a minimum pressure margin, the outer, main and internal redundancy panels being separated from one another by spaces (5, 6). The invention also relates to an aircraft comprising windscreen elements and portholes made using the glass panel.


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    Title :

    Glass panel for a space aircraft


    Contributors:

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



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