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.

    A landing apparatus for a reusable launch vehicle is provided, including a landing leg pivotably mounted at one end to the reusable launch vehicle, for example, to a propellant tank part, and mounted at the other end to the propellant tank part by a detaching means such as a pyro bolt for example, a cover mounted to an outside of the landing leg along a longitudinal direction of the landing leg, and a leg landing plate mounted to a distal end of the landing leg and relatively pivotable with respect to the landing leg by its own weight when the other end of the landing leg is separated from the propellant tank part.


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    Titel :

    Landing apparatus for reusable launch vehicle


    Weitere Titelangaben:

    재사용 발사체 착륙장치


    Erscheinungsdatum :

    13.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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