The present invention relates to a reusable projectile which can be reused like an aircraft by returning to the ground after transporting cargo from the ground to a space orbit or a space place and, more specifically, to a non-separable pairing opening and closing structure for a reusable projectile and a reusable projectile including the same, capable of reusing pairing separated from the projectile.

    본 발명은 지상에서 우주궤도 또는 우주공간까지 화물을 운송한 후 지상으로 복귀하여 항공기처럼 재사용이 가능한 재사용 발사체에 관한 것으로, 더욱 상세하게는 발사체에서 분리되는 페어링도 재사용이 가능하도록 한 재사용 발사체 용 비분리식 페어링 개폐 구조 및 이를 포함하는 재사용 발사체에 관한 것이다.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Reusable Launch Vehicle having Fairing Open-and-Close Mechanism and Operating Method of the Same


    Weitere Titelangaben:

    비분리식 페어링 개폐 구조를 포함하는 재사용 발사체 및 이의 운용 방법


    Beteiligte:
    SHIN DONG YOON (Autor:in) / HWANG DAEHYUN (Autor:in)

    Erscheinungsdatum :

    27.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    REUSABLE LAUNCH VEHICLE COMPRISING NON-SEPARABLE FAIRING OPENING/CLOSING STRUCTURE, AND OPERATING METHOD THEREOF

    SHIN DONG YOON / HWANG DAEHYUN | Europäisches Patentamt | 2025

    Freier Zugriff

    Low cost launch vehicle fairing

    TURNER ANDREW E / HART III WILLIAM G | Europäisches Patentamt | 2019

    Freier Zugriff

    Reusable fairing structure

    BAO YUBING / WANG SHUFAN / CHEN YOUWEI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Optimum Launch Vehicle Fairing: An MDO Approach

    Colonno, M. / Alonso, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Optimum Launch Vehicle Fairing: An MDO Approach

    Colonno, Michael / Alonso, Juan | AIAA | 2008