The invention discloses a transition plate structure for flexible spacecraft storage. Due to the fact that the non-flexible spacecraft is basically adopted in the prior art, the structure of the non-flexible spacecraft has certain rigidity, displacement changes cannot happen, the size of the non-flexible spacecraft device and the size of the data transmission and power supply system device cannotchange any more after the non-flexible spacecraft device and the data transmission and power supply system device are installed and fixed, so that the non-flexible spacecraft device and the power supply system device are integrated in one box. However, because the flexible spacecraft is adopted and needs to be stored and fixed after being installed due to inherent flexibility of the flexible spacecraft, and if the flexible spacecraft is fixed in a box in the prior art, unfolding of the flexible spacecraft cannot be achieved, the invention provides a novel flat satellite structure of a transition plate. The transition plate has the advantages of low cost, high functional density and short development period.
本发明公开了一种用于柔性航天器收纳的过渡板结构。由于现有技术基本是采用非柔性航天器,其结构本身具有一定的刚性,不会发生位移变化,非柔性航天器装置与其数传及电源系统装置安装固定后体积不会再发生变化,故通常二者集成在一个盒子里即可。但本发明由于采用的是柔性航天器,因其本身固有柔性,需要在安装后对其进行收纳固定,而若采用现有技术,将其固定在一个盒子里,则无法实现柔性航天器的展开,为此本发明提供了一种过渡板的新型平板卫星结构,具有成本低、功能密度大、研制周期短的优点。
Transition plate for flexible spacecraft storage
一种用于柔性航天器收纳的过渡板
2021-04-02
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Spacecraft flexible storage container and construction method
Europäisches Patentamt | 2020
|NTRS | 1987
NTIS | 1987