The invention provides a 6U cubesat with a standardized platform. The 6U cubesat is novel in structural design, integrated and capable of realizing standardized application, and comprises a management unit, a battery pack unit, an X measurement and control and data transmission unit, an attitude control unit and a frame structure, the battery pack unit, the X measurement and control and data transmission unit and the attitude control unit are sequentially arranged from top to bottom to form a platform mounting unit, the platform mounting unit is mounted on one side in the frame structure, and an internal area of the other side in the frame structure at the side part of the platform mounting unit is a cavity to form a load bin; a data transmission antenna, a remote control antenna and a telemetering antenna are installed on the side wall of the near-ground side of the frame structure; and solar wing cell array assemblies are installed on the two side edges of the side wall of the sun facing side of the frame structure respectively, and one side edge of each solar wing cell array assembly is connected with the side edge of the frame structure of the side wall of the sun facing side through a hinge mechanism.
本发明提供一种结构设计新颖、集成化可实现标准化应用的具备标准化平台的6U立方星,包括管理单元、电池组单元、X测控与数传单元、姿控单元、框架结构,所述电池组单元、X测控与数传单元、姿控单元由上至下依次设置构成平台安装单元安装于所述框架结构内的一侧,所述平台安装单元侧部的所述框架结构内的另一侧内部区域为空腔构成载荷仓;所述框架结构近地侧的侧壁上安装有数传天线、遥控天线、遥测天线;所述框架结构对日侧的侧壁两侧边上分别安装有太阳翼电池阵组件,所述太阳翼电池阵组件的一侧边通过铰链机构与所述对日侧的侧壁框架结构侧边连接。
6U cubesat with standardized platform
具备标准化平台的6U立方星
2021-11-02
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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