The invention relates to a remote sensing load and satellite integrated configuration, which comprises a satellite body and a camera load, and is characterized in that the satellite body comprises a top plate, a middle plate and a bottom plate, the top plate, the middle plate and the bottom plate are sequentially arranged in parallel at intervals, the top plate and the middle plate are fixedly connected through an upper frame, and the middle plate and the bottom plate are fixedly connected through a lower frame; a first through hole is formed in the center of the top plate, a second through hole is formed in the center of the middle plate, and a third through hole is formed in the center of the bottom plate; an inner cylinder is arranged in the axial center of the satellite body, the inner cylinder is of a hollow structure with the two ends open, the upper end of the inner cylinder is fixed to a top plate of the satellite body and communicates with the first through hole, and the lower end of the inner cylinder is fixed to a middle plate of the satellite body and communicates with the second through hole; and the lower end of the camera load is fixedly supported on the bottom plate, and the camera load is located on the inner sides of the first through hole, the second through hole, the third through hole and the inner cylinder.
本发明涉及一种遥感载荷与卫星的一体化构型,包括卫星本体和相机载荷,所述卫星本体包括顶板、中板和底板,所述顶板、中板和底板依次平行间隔布置,所述顶板和中板之间通过上框架固定连接,所述中板与底板之间通过下框架固定连接;所述顶板的中心位置开设有第一通孔,所述中板的中心位置开设有第二通孔,所述底板的中心位置开设有第三通孔;所述卫星本体轴向的中心位置设有内筒,所述内筒为两端敞口的中空结构,所述内筒的上端固定在所述卫星本体的顶板上且与第一通孔连通,所述内筒的下端固定在所述卫星本体的中板上且与第二通孔连通;所述相机载荷的下端固定支撑在所述底板上,所述相机载荷位于第一通孔、第二通孔、第三通孔以及内筒的内侧。
Integrated configuration of remote sensing load and satellite
一种遥感载荷与卫星的一体化构型
2023-05-09
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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