The invention provides a micro-nano satellite platform. The micro-nano satellite platform comprises a structure module, a thermal control module, an information module, a power supply and distribution module and an attitude and orbit control module, the thermal control module, the information module, the power supply and distribution module and the attitude and orbit control module are assembled on the surface of the structure module; the thermal control module, the information module, the power supply and distribution module and the attitude and orbit control module are electrically connected with one another; the structure module is used for installing and arranging instruments and equipment on a satellite; the thermal control module is used for providing a heat sealing environment; the information module is used for information control, processing and transmission; the power supply and distribution module is used for supplying power to a satellite; and the attitude and orbit control module is used for controlling the attitude of the satellite. The launching mode provided by the invention is flexible, adapts to and is compatible with multiple types of carrier rockets, and can be positively mounted and laterally hung on the carrier rockets by adjusting the layout position of the separation mechanism on the satellite, so that rapid networking deployment of low-orbit constellations is facilitated.
本发明提供了一种微纳卫星平台,包括:结构模块、热控模块、信息模块、供配电模块、姿轨控模块;所述热控模块、所述信息模块、所述供配电模块与所述姿轨控模块,装配在所述结构模块的表面上;所述热控模块、所述信息模块、所述供配电模块与所述姿轨控模块彼此之间通过电气连接;所述结构模块,用于安装布局卫星上的仪器与设备;所述热控模块,用于提供合热环境;所述信息模块,用于信息控制、处理与传输;所述供配电模块,用于为卫星供能;所述姿轨控模块,用于控制卫星的姿态。本发明提供的发射方式灵活,适应兼容多型运载火箭,通过调整分离机构在星上的布局位置,既能够正装也能够侧挂在运载火箭上,有利于低轨星座的快速组网部署。
Micro-nano satellite platform
微纳卫星平台
2024-12-03
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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