The invention discloses a box plate and frame combined type satellite configuration, and relates to the technical field of satellites. The box plate and frame combined type satellite configuration comprises a platform cabin, a load cabin and a sailboard; the load cabin is located at the top of the platform cabin; the platform cabin comprises a platform box body and a platform frame structure; the load cabin comprises a load plate, a load frame structure and a load truss structure; the platform frame structure is arranged in the platform box body, the bottom of the platform frame structure is connected with the platform box body, and the top of the platform frame structure is connected with the load plate; the outer side face of the load frame structure is connected with the sailboard, and the inner side face of the load frame structure is connected with the load truss structure; the load frame structure and the load truss structure are both connected with the top of the load plate; and the bottom of the platform box body is connected with a butt joint ring. The invention aims to provide the box plate and frame combined type satellite configuration, so that the universal performance is improved to a certain extent, different customization requirements are met, and the box plate and frame combined type satellite configuration can be further suitable for satellites of various load types.
一种箱板框架组合式卫星构型,涉及卫星技术领域。该箱板框架组合式卫星构型包括平台舱、载荷舱和帆板;载荷舱位于平台舱的顶部;平台舱包括平台箱体和平台框架结构;载荷舱包括载荷板、载荷框架结构和载荷桁架结构;平台框架结构设置在平台箱体的内部,且平台框架结构的底部与平台箱体连接,平台框架结构的顶部与载荷板连接;载荷框架结构的外侧面与帆板连接,载荷框架结构的内侧面与载荷桁架结构连接;载荷框架结构和载荷桁架结构均与载荷板的顶部连接;平台箱体的底部连接有对接环。本发明的目的在于提供一种箱板框架组合式卫星构型,以在一定程度上提高通用性能、满足不同的定制化需求,进而能够适用于多种载荷类型的卫星。
Box plate and frame combined type satellite configuration
箱板框架组合式卫星构型
2021-10-29
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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