The invention provides a folding flat satellite configuration. The folding flat satellite configuration is designed; a folding flat satellite body comprises a first satellite cabin body and a second satellite cabin body; a connector used for connecting the first satellite cabin body and the second satellite cabin body is arranged; angles between opposite sky surfaces of the first satellite cabin body and the second satellite cabin body can be adjusted; and the two cabins of the satellite can be folded or unfolded so as to be placed in a fairing in a stacked mode and adapt to different fairingsizes, a extremely high fairing space utilization rate is achieved, ''one-rocket multi-satellite'' launching with a high numerical proportion is achieved, rapid and low-cost deployment of satellite constellation is guaranteed, and therefore the two problems of satellite launching period requirements and cost control requirements are solved. And the configuration has characteristics of a large ground area and multiple heat dissipation surfaces, and is more friendly to a satellite design taking space-based radar remote sensing, high-capacity satellite communication and other microwave applications as main directions.
本发明提供一种折叠式平板卫星构型,通过对折叠式平板卫星构型的设计,所述折叠式平板卫星本体包括第一卫星舱体和第二卫星舱体,并且通过设置用于连接所述第一卫星舱体和第二卫星舱体的连接器,使所述第一卫星舱体和第二卫星舱体各自的对天面之间的角度可调节,进而卫星的两个舱体可以折叠或者展开,从而可以在整流罩内以层叠堆放的方式放置,能够适应不同整流罩尺寸,达到极高的整流罩空间利用率,既实现高数值比例的“一箭多星”发射,又保证卫星星座的快速、低成本部署,从而解决卫星发射周期需求和成本控制需求两大难题。且具有对地面大,散热面多的特点,对以天基雷达遥感、大容量卫星通信等微波应用为主要方向卫星设计更友好。
Folding flat satellite configuration
折叠式平板卫星构型
2020-10-13
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |