FIELD: astronautics.SUBSTANCE: invention relates to rocket engineering. Aerodynamic steering wheel of a hypersonic aircraft contains a spar, a skin and a plate made of heat-conducting material with a melting point below the melting point of the skin that is spring loaded from the side member to the leading edge. Plate has a surface coating of a material having a melting point below the melting point of the plate material. Internal cavity of the skin has grooves for removal of the melted material of the plate.EFFECT: invention is aimed at improving the reliability of the structure during aerodynamic heating.1 cl, 1 dwg


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    Titel :

    РУЛЬ АЭРОДИНАМИЧЕСКИЙ ГИПЕРЗВУКОВОГО ЛЕТАТЕЛЬНОГО АППАРАТА В УСЛОВИЯХ ЕГО АЭРОДИНАМИЧЕСКОГО НАГРЕВА


    Erscheinungsdatum :

    15.02.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge