PROBLEM TO BE SOLVED: To provide a rocket assembly launch facility capable of omitting an opening/closing door to significantly reduce a construction cost and a maintenance cost for the rocket launch facility.SOLUTION: A rocket assembly launch facility comprises: an assembly building 20 including an assembly chamber used for assembly and maintenance of the rocket airframe A; and a launch facility 30. A projection opening 23, a shape of which is the same as a projected shape of the launch facility, is formed in a front face 20a of the assembly building 20, either one or both of the assembly building 20 and the launch facility 30 are configured to be movable, and the projection opening 23 of the assembly building 20 and the launch facility 30 are configured to be fitted together.SELECTED DRAWING: Figure 1

    【課題】組立棟の開閉用扉を省略できて、ロケット射場設備の建設費用と維持費の大幅低減が可能なロケット射場設備を提供すること。【解決手段】ロケット機体Aの組み立てと整備を行う組立室を有する組立棟20と、発射台装置30とを具備し、組立棟20の前面20aに発射台装置の投影形状と同形の投影口23を形成し、組立棟20、発射台装置30の何れか一方の設備、又は両設備を走行可能に構成すると共に、組立棟20の投影口23と発射台装置30とを嵌合可能に構成した。【選択図】図1


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    Titel :

    ROCKET ASSEMBLY LAUNCH FACILITY


    Weitere Titelangaben:

    ロケット組立発射設備


    Beteiligte:
    OKURA HIROTAKA (Autor:in) / HOGEN NAOSHIGE (Autor:in) / KAMIYA TAKASHI (Autor:in)

    Erscheinungsdatum :

    2016-07-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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