The invention provides a high-stability large-scale remote sensing satellite platform. The high-stability large-scale remote sensing satellite platform comprises three parts: a bearing cylinder, a platform cabin and a load adaptive structure, wherein the platform cabin wraps the outer side of the force bearing cylinder in a non-closed mode, and the load adaptation structure is fixed to the upper portion of the force bearing cylinder. The platform cabin is of a plate type structure and is not fixedly connected with the load adaptation structure, and the bottom of the force bearing cylinder is used for being connected with a carrier rocket. When the platform is designed, the load adaptive structure is directly and fixedly connected with the force bearing cylinder, the load adaptive structure is not connected with other structures of the satellite platform, the force transmission of the whole spacecraft takes the force bearing cylinder as a core, and the load generated by an effective load is transmitted to the force bearing cylinder through the load adaptive structure and then transmitted to a carrier.
本发明提供一种高稳定大型遥感卫星平台,包括三部分:承力筒、平台舱及载荷适配结构;其中所述平台舱非封闭的包裹于承力筒的外侧,所述载荷适配结构固定于承力筒的上方;所述平台舱为板式结构,其与所述载荷适配结构之间不固连,承力筒的底部用于连接运载火箭。该平台设计时载荷适配结构与承力筒直接固连,载荷适配结构与卫星平台的其他结构不连接,整个航天器的传力以所述承力筒为核心,有效载荷产生的载荷经过所述载荷适配结构到所述承力筒再传到运载。
High-stability large remote sensing satellite platform
一种高稳定大型遥感卫星平台
2023-05-02
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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