The invention provides a compact satellite configuration suitable for multi-band detection load, which comprises a satellite body, a double-wing solar cell assembly, a relay antenna, a multi-band detection load antenna module, a communication load module, a data transmission antenna module, a measurement and control antenna and a thruster, wherein a left-wing solar cell array and a right-wing solar cell array in the double-wing solar cell assembly are installed on the left side face and the right side face of the satellite body respectively; the relay antenna and the multi-band detection loadantenna assembly are installed on the back and the front of the satellite body respectively; the communication load assembly and the thruster are both installed on the satellite body; a left data transmission antenna and a right data transmission antenna in the data transmission antenna assembly are installed on the left side face and the right side face of the satellite body respectively; the measurement and control antenna is installed on the front and/or back of the satellite body. The structure is compact, good manufacturability and high integration of satellites are achieved, and the on-orbit application requirements of the satellites are met.
本发明提供了一种适用于多频段探测载荷的紧凑型卫星构型,包括卫星本体、双翼太阳电池组件、中继天线、多频段探测载荷天线组件、通信载荷组件、数传天线组件、测控天线以及推力器,双翼太阳电池组件中的左翼太阳电池阵、右翼太阳电池阵分别安装在卫星本体的左侧面、右侧面;中继天线、多频段探测载荷天线组件分别安装在卫星本体的背面、正面;通信载荷组件、推力器都安装在卫星本体上;数传天线组件中的左数传天线、右数传天线分别安装在卫星本体的左侧面、右侧面上;测控天线安装在卫星本体的正面和/或背面。本发明构型紧凑,实现卫星的良好工艺性和高度集成化,满足卫星在轨应用需求。
Compact satellite configuration suitable for multi-band detection load
适用于多频段探测载荷的紧凑型卫星构型
2020-11-06
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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