The invention provides a satellite configuration loaded with a deployable antenna and a satellite. The satellite configuration loaded with the deployable antenna comprises a platform cabin, a load cabin truss, the deployable antenna, a solar array, a data transmission antenna and a star sensor, the platform cabin is connected with the load cabin truss, and the solar array and the deployable antenna are installed on the two sides, in the same direction, of the platform cabin and the load cabin truss respectively. A data transmission antenna is installed on one side face, located between the solar arrays on the two sides, of the platform cabin, and the star sensor is installed on the load cabin truss. The unfolding direction of the deployable antenna is perpendicular to the longitudinal direction of the load cabin truss, that is, the longitudinal direction of the deployable antenna is parallel to the longitudinal direction of the satellite, the longitudinal size of the deployable antenna can be greatly increased, and therefore the deployable antenna can adapt to installation of a large-area deployable antenna in a one-dimensional folding and unfolding mode.
本发明提供了一种装载可展开天线的卫星构型及卫星,包括:平台舱、载荷舱桁架、可展开天线、太阳阵、数传天线以及星敏感器;所述平台舱连接所述载荷舱桁架,所述平台舱和所述载荷舱桁架同一方向的两侧分别安装太阳阵和可展开天线;所述平台舱位于两侧太阳阵之间的一侧面上安装数传天线,所述星敏感器安装在所述载荷舱桁架上。本申请采用可展开天线的展开方向与载荷舱桁架纵向垂直,即可展开天线的纵向与卫星纵向平行,可大大增加可展开天线纵向的尺寸,从而可适应一维折叠展开方式下的大面积可展开天线的安装。
Satellite configuration loaded with deployable antenna and satellite
装载可展开天线的卫星构型及卫星
2025-01-03
Patent
Electronic Resource
Chinese