PROBLEM TO BE SOLVED: To provide a missile with an ablator which is secured in heat protection characteristics while maintaining the strength.SOLUTION: A missile comprises a high fiber density ablator part 5 which is provided on an external surface S side of a body and is mainly composed of resin and a fiber matrix, and low fiber density ablator parts 7 which have a lower fiber density than that of the high fiber density ablator part 5 and are mainly composed of resin and a fiber matrix. The high fiber density ablator part 5 is formed with grooves 9, and the low fiber density ablator parts 7 are formed in the grooves 9. The grooves 9 are in communication with an external surface S.SELECTED DRAWING: Figure 2

    【課題】強度を維持しつつ熱防護性が確保されたアブレータ材を備えた飛昇体を提供する。【解決手段】本体の外表面S側に設けられ、樹脂と繊維マトリックスを主成分とする高繊維密度アブレータ部5と、高繊維密度アブレータ部5よりも低繊維密度とされ、樹脂と繊維マトリックスを主成分とする低繊維密度アブレータ部7とを備え、高繊維密度アブレータ部5には、溝9が形成され、低繊維密度アブレータ部7は、溝9に設けられ、溝9は、外表面Sに連通していることを特徴とする。【選択図】図2


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    Titel :

    MISSILE


    Weitere Titelangaben:

    飛昇体


    Beteiligte:
    FUJIO KAZUSUKE (Autor:in) / TAJIRI SHINSUKE (Autor:in) / MORIWAKI ATSUSHI (Autor:in) / FUKUDA HIROSHI (Autor:in) / ANDO KEISUKE (Autor:in) / UKAI HIRONORI (Autor:in)

    Erscheinungsdatum :

    18.05.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B64C AEROPLANES , Flugzeuge / F16L PIPES , Rohre



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