The invention relates to a modular multifunctional satellite configuration which comprises an integrated flat plate, a peripheral frame, a reinforcing frame, four bearing columns and externally-hung side cabins, the integrated flat plate and the reinforcing frame are arranged in the peripheral frame, the number of the externally-hung side cabins is 1-4, the number of the bearing columns is 4, multiple satellites can be stacked in a multi-layer mode through the bearing columns, and the satellites have two stacking modes. One is that four bearing columns between the upper and lower satellites are coaxially stacked; according to the second structure, two force bearing columns between the upper-layer satellite and the lower-layer satellite are coaxially stacked, the other two force bearing columns are provided with compensation columns between the upper-layer satellite and the lower-layer satellite, and the height of the compensation columns adapts to the stacking height design of the interlayer satellites. According to the invention, the engineering requirements of different satellite equipment mounting areas, fairing carrying states and a one-rocket multi-satellite launching mode can be met, a cable mounting bracket does not need to be additionally arranged, the cable network mounting process is simplified, and convenience is provided for batch final assembly of the cable network.
本发明涉及一种模块化多功能卫星构型,包括一体化平板、外围框架、加强框架、承力柱和外挂侧舱,一体化平板和加强框架设置在外围框架内,外挂侧舱数目为1‑4,承力柱数目为4,多颗卫星可通过承力柱多层叠放,卫星具备两种叠放方式,其一为上下层卫星之间4处承力柱同轴叠放;其二为上下层卫星之间2处承力柱同轴叠放,另2处承力柱在上下层卫星之间设置补偿柱,补偿柱高度适应层间卫星叠放高度设计。本发明可满足不同卫星设备安装面积、运载整流罩状态、一箭多星发射方式的工程需求,无需额外设置电缆安装支架,简化了电缆网安装工艺,为电缆网批量化总装提供了便利。
Modularized multifunctional satellite configuration
一种模块化多功能卫星构型
25.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |