The invention provides a communication satellite structure and a carrier rocket, and relates to the technical field of satellites. The communication satellite structure provided by the invention comprises box body plates, wherein the box body plates form a trapezoidal box body structure; the partition plates are arranged in the box body plate at intervals, and the partition plates and the inner wall of the box body plate form a single machine mounting surface; and the main bearing corner box is arranged at least one of the corner of the box body plate and the position between the partition plate and the box body plate. According to the invention, through the hollow trapezoidal box body structure formed by the box body plates, the communication satellite structure is light in weight, the space utilization rate is improved, and the number of the communication satellite structures which can be carried by a carrier rocket is increased, so that batch and large-scale launching of the communication satellite structures is realized; the overall rigidity and strength of the communication satellite structure are improved through the partition plates and the main bearing corner boxes, and meanwhile the area of a single-machine installation face is increased, so that satellite single-machine installation is facilitated.
本申请提供一种通信卫星结构及运载火箭,涉及卫星技术领域。本申请提供的通信卫星结构包括箱体板,箱体板构成梯形箱体结构;隔板,间隔设置于箱体板的内部,隔板与箱体板的内壁形成单机安装面;主承力角盒,设置于箱体板的边角处和隔板与箱体板之间处的至少之一。本申请通过箱体板构成的内部中空的梯形箱体结构,使通信卫星结构轻量化,提高空间利用率,增大运载火箭可搭载的通信卫星结构数量,以助于实现通信卫星结构的批量大规模发射;通过隔板和主承力角盒以增大通信卫星结构整体的刚性和强度,同时增大了单机安装面的面积,以便于卫星单机的安装。
Communication satellite structure and carrier rocket
通信卫星结构及运载火箭
2024-10-01
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |