The invention discloses a microsatellite configuration suitable for batch production and an assembly method, and belongs to the technical field of spacecrafts. The microsatellite configuration comprises a satellite main body, a satellite bottom plate module is installed at the bottom of the satellite main body, a satellite electronics module is installed and connected to the rear side of the satellite main body, satellite Y plates are installed on the two sides of the satellite main body respectively, and the satellite Y plates are fixedly connected with the two sides of the satellite electronics module respectively; a satellite X plate is mounted and connected to the front side of the satellite main body; the two sides of the satellite Y plate are connected with solar wings respectively. The modular design is adopted, and the satellite is designed into two parts, namely an electronics module and a bottom plate module. Satellite assembly chains are parallel, the total operation time is shortened, satellite maintainability is improved, and operation is easier and more convenient.
本发明公开了一种适用批产的微小卫星构型及装配方法,属于航天器技术领域。所述微小卫星构型,包括:卫星主体,所述卫星主体底部安装有卫星底板模块,所述卫星主体后侧安装连接有卫星电子学模块,所述卫星主体两侧分别安装有卫星Y板,所述卫星Y板与卫星电子学模块两侧分别连接固定;所述卫星主体前侧安装连接有卫星X板;所述卫星Y板两侧分别连接有太阳翼。本发明采用模块化设计,将卫星设计为电子学模块和底板模块两部分。使卫星总装链条并行,减少总的操作时间,提高卫星维修性,操作更为简便。
Microsatellite configuration suitable for batch production and assembly method
一种适用批产的微小卫星构型及装配方法
2024-05-14
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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