The invention provides a carrier rocket which is small in transmission error, large in motion rigidity and high in bearing capacity and a pose adjusting structure thereof. The pose adjusting structure of the carrier rocket comprises a rocket cabin body, and a first mounting hole is formed in the rocket cabin body; a mounting frame is arranged on the inner wall of the rocket cabin body and is positioned at the first mounting hole; a rudder surface and a rudder shaft are connected with each other, and the rudder shaft penetrates through the first mounting hole and then is rotatably connected with the mounting frame; and a driving mechanism is arranged on the rocket cabin body and drives the rudder shaft to rotate.

    本发明提供了一种传递误差小、运动刚度大、承载能力强的运载火箭及其位姿调整结构。其中,运载火箭的位姿调整结构包括火箭舱体,火箭舱体上设置有第一安装孔;安装架,设置在火箭舱体的内壁上并位于第一安装孔处;互相连接的舵面以及舵轴,舵轴穿过第一安装孔后可转动地连接在安装架上;驱动机构,设置在火箭舱体上并驱动舵轴转动。


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    Title :

    Carrier rocket and pose adjusting structure thereof


    Additional title:

    运载火箭及其位姿调整结构


    Contributors:
    PENG XIAOBO (author) / CUI SHENSHAN (author) / ZHANG XIAOFEI (author) / HUANG ZHICHENG (author) / LIU PENGCHENG (author) / YANG XIAOSHUN (author)

    Publication date :

    2021-04-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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