The invention relates to a platform and load integrated satellite structure suitable for a multi-module splicing load, and relates to the technical field of spaceflight satellites. The system comprises a satellite structure and an effective load. The satellite structure comprises a butt joint ring, a platform bottom plate, a first platform long partition plate, a second platform long partition plate, a first platform short partition plate, a second platform short partition plate, a third platform short partition plate, a fourth platform short partition plate, a first platform small partition plate, a second platform small partition plate, four platform supporting beams, a load cabin large bottom plate, a load cabin small bottom plate, a first load mounting plate, a second load mounting plate and a third load mounting plate. The load cabin comprises a first load cabin small top plate, a second load cabin small top plate, four first load supporting beams, four second load supporting beams, a first side plate, a second side plate, a third side plate and a fourth side plate. And the effective load comprises five effective load modules I, five effective load modules II and three effective load modules III.
本发明涉及一种适用于多模块拼接载荷的平台与载荷一体化卫星结构,涉及航天卫星技术领域。本发明包括卫星结构和有效载荷;卫星结构包括对接环、平台底板、平台长隔板一、平台长隔板二、平台短隔板一、平台短隔板二、平台短隔板三、平台短隔板四、平台小隔板一、平台小隔板二、四个平台支撑梁、载荷舱大底板、载荷舱小底板、载荷安装板一、载荷安装板二、载荷安装板三、载荷舱小顶板一、载荷舱小顶板二、四个载荷支撑梁一、四个载荷支撑梁二、侧板一、侧板二、侧板三、侧板四;有效载荷包括五台有效载荷模块一,五台有效载荷模块二,三台有效载荷模块三。
Platform and load integrated satellite structure suitable for multi-module splicing load
一种适用于多模块拼接载荷的平台与载荷一体化卫星结构
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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