According to an embodiment of the present invention, provided is a reusable projectile landing gear including: a landing leg, one end of which is rotatably mounted on a propellant tank part of a reusable projectile and the other end is mounted on the propellant tank part with a pyro bolt; a cover mounted on the outside of the landing leg along the longitudinal direction of the landing leg; and a leg landing plate which is mounted at the end of the landing leg, and is capable of rotating relative to the landing leg by its own weight when the other end of the landing leg is separated from the propellant tank part.

    본 발명의 한 실시예에 따른 재사용 발사체 착륙장치는 재사용 발사체의 추진제 탱크부에 일단부가 회동 가능하게 장착되고, 타단부는 파이로 볼트(pyro bolt)로 상기 추진제 탱크부에 장착된 랜딩 레그(landing leg), 상기 랜딩 레그의 길이방향을 따라 상기 랜딩 레그의 외측에 장착된 커버, 그리고 상기 랜딩 레그의 말단에 장착되고, 상기 랜딩 레그의 타단부가 상기 추진제 탱크부로부터 분리될 때, 자중에 의하여 상기 랜딩 레그에 대해 상대적으로 회동 가능한 레그 착륙판을 포함하는 것을 특징으로 한다.


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    Titel :

    Landing apparatus for reusable launch vehicle


    Weitere Titelangaben:

    재사용 발사체 착륙장치


    Beteiligte:
    JUNG DONG HO (Autor:in)

    Erscheinungsdatum :

    2023-03-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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