Platform and load integrated design satellite load cabin

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Platform and load integrated design satellite load cabin

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YAO YANFENG / LI FENG / PEI SHENGWEI / GAO YOUDAO / HAO YANYAN / DENG YUHUA / FAN WEI / WANG MIAN / LIU BING

The invention relates to a platform and load integrated design satellite load cabin, and belongs to the field of spaceflight technology and equipment. The south plate, the east plate, the north plate and the west plate are sequentially butted end to end to define a square cavity structure; the grounding plate horizontally covers the top of the square cavity structure; the external space camera is arranged at the center of the upper surface of the floor; the middle partition plate is vertically arranged in an inner cavity of the square cavity structure. The two axial ends of the east partition plate are in butt joint with the middle of the east plate and the middle of the middle partition plate correspondingly. The west clapboard is vertical to the middle clapboard; every two of the four heat conduction pipes form a group, and the two groups of heat conduction pipes are butted to form a U-shaped heat conduction pipe group; the load cabin is compact in structure, the supporting and heat dissipation requirements of a space camera structure and satellite design are considered as a whole, the structure and thermal control advantages of the whole satellite are fully played, the integrated design of the space camera and the satellite structure and thermal control is achieved, and the requirements for reliable supporting and high-precision temperature control of the space camera are met.

本发明涉及一种平台和载荷集成设计卫星载荷舱，属于航天技术和设备领域；南板、东板、北板、西板依次首尾对接围成正方形腔体结构；对地板水平盖在正方形腔体结构的顶部；外部空间相机设置在对地板上表面的中心处；中隔板竖直设置在正方形腔体结构的内腔中；东隔板垂直于中隔板，且东隔板的轴向两端分别与东板的中部、中隔板的中部对接；西隔板垂直于中隔板；4个导热管两两一组，两组导热管对接呈U型导热管组；本发明载荷舱结构紧凑，将空间相机结构支撑和散热需求与卫星设计统筹考虑，充分发挥整星结构和热控优势，实现了空间相机与卫星结构和热控一体化设计，满足空间相机可靠支撑和高精度温度控制的要求。

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Titel :

Platform and load integrated design satellite load cabin

Weitere Titelangaben:

一种平台和载荷集成设计卫星载荷舱

Beteiligte:

YAO YANFENG (Autor:in) / LI FENG (Autor:in) / PEI SHENGWEI (Autor:in) / GAO YOUDAO (Autor:in) / HAO YANYAN (Autor:in) / DENG YUHUA (Autor:in) / FAN WEI (Autor:in) / WANG MIAN (Autor:in) / LIU BING (Autor:in)

Erscheinungsdatum :

2022-07-08

Medientyp :

Patent

Format :

Elektronische Ressource

Sprache :

Chinesisch

Klassifikation :

IPC:

B64G Raumfahrt , COSMONAUTICS

Platform and load integrated design satellite load cabin

Platform and load integrated design satellite load cabin

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