PROBLEM TO BE SOLVED: To suppress adverse effect such as acoustic excitation on a payload caused by reflection sound of injection sound generated by a combustion gas injection port without an increase in dead weight of a rocket at rocket launching.SOLUTION: A rocket launch facility includes a vertical support part for installing a rocket 10 in a vertical state. The rocket launch facility includes a surface P facing the combustion gas injection port provided in a rear part of the rocket when the rocket is installed thereto vertically. The surface is formed so as to be directed downward as receding from a shaft center O of the rocket.SELECTED DRAWING: Figure 1

    【課題】ロケット打ち上げ時にロケットの自重を増すことなく、燃焼ガス噴射口で発生する噴射音の反射音が搭載物を音響加振するなどの悪影響を抑制する。【解決手段】ロケット10を垂直状態で設置する垂直支持部を有するロケット発射設備であって、前記ロケット発射設備は、前記ロケットが垂直に支持されたとき、前記ロケットの後部に設けられた燃焼ガス噴射口と対面する面Pを有し、前記面は、前記ロケットの軸中心Oから遠ざかるにつれて下方へ向かうように形成されている。【選択図】図1


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    Title :

    ROCKET LAUNCH FACILITY AND ROCKET LAUNCH METHOD


    Additional title:

    ロケット発射設備及びロケット発射方法


    Contributors:

    Publication date :

    2016-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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