The invention provides a business cubesat configuration suitable for multiple separation modes and an assembly method, and belongs to the field of satellite design. The problems that an existing cubesat is single in separation mode and few in carrying opportunities are solved. The device comprises a whole satellite frame, expandable solar wings, an in-cabin single machine, an out-cabin single machine and a separation assembly, the in-cabin single machine is arranged in the whole satellite frame, the expandable solar wings, the out-cabin single machine and the separation assembly are all arranged outside the whole satellite frame, and the two groups of expandable solar wings are arranged and installed on a + Y single machine plate and a-Y single machine plate respectively; the in-cabin single machine comprises a flywheel, a propeller, a gyroscope, a star sensor, a large comprehensive power system, a storage battery and a camera assembly; the outboard assembly is installed on the + Z single machine plate, two separation guide rails are arranged at the front end and the rear end of the + Y single machine plate, two separation guide rails are arranged at the front end and the rear end of the-Y single machine plate, and the separation assembly is installed on the separation guide rails or the-Z single machine plate. The method is suitable for various satellite-rocket separation modes, and the satellite carrying and launching opportunities are increased.
本发明创造提供了一种适用于多种分离方式的业务化立方星构型及装配方法,属于卫星设计领域。解决了现有立方星分离方式单一、搭载机会少问题。它包括整星框架、可展开太阳翼、舱内单机、舱外单机和分离组件,舱内单机设置在整星框架内部,可展开太阳翼、舱外单机和分离组件均设置在整星框架的外部,可展开太阳翼设置两组,分别安装在+Y单机板和‑Y单机板上;舱内单机包括飞轮、推进、陀螺、星敏、大综电系统、蓄电池和相机组件;舱外组件安装在+Z单机板上,+Y单机板的前后两端设置两根分离导轨,‑Y单机板的前后两端设置两根分离导轨,分离组件安装在分离导轨或‑Z单机板上。本发明创造适用于多种星箭分离方式,增加卫星搭载发射机会。
Business cubesat configuration suitable for multiple separation modes and assembly method
一种适用于多种分离方式的业务化立方星构型及装配方法
01.11.2022
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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