The invention discloses a carrying service-oriented satellite platform configuration, belongs to the technical field of satellite structures, and aims to solve the problems that in the prior art, the mounting requirements of multiple types of loads cannot be met, the carrying efficiency is low, the research and development period is long, and the research and development cost is high. The device comprises a carbon fiber bearing cylinder located in the middle and a camera mounting plate arranged at one end of the carbon fiber bearing cylinder, and an optical load is mounted on the camera mounting plate and located in the carbon fiber bearing cylinder; the carrying plate is arranged on the upper side surface of the carbon fiber bearing cylinder; the two solar wing sailboards are symmetrically arranged on the left side surface and the right side surface of the carbon fiber bearing cylinder about the center of mass of the satellite platform configuration; the platform single machine is mounted on the left cabin plate and the carbon fiber bearing cylinder; a plurality of carrying single machines installed in the carrying area of the carrying board; the high-power-consumption single machine is mounted on the right side surface of the carbon fiber bearing cylinder; the separation mechanism is mounted on the lower side surface of the carbon fiber bearing cylinder; and the propeller is mounted on the lower side surface of the carbon fiber bearing cylinder.
本发明公开一种面向搭载业务的卫星平台构型,属于卫星结构技术领域,目的在于解决现有技术存在的无法满足多类型载荷的安装需求、搭载效率低、研发周期长以及研发成本高的问题。本发明包括:位于中部的碳纤维承力筒,设置在碳纤维承力筒一端部的相机安装板,光学载荷安装在相机安装板上,并位于碳纤维承力筒内;设置在碳纤维承力筒上侧面的搭载板;关于卫星平台构型质心对称设置在碳纤维承力筒左侧面和右侧面的两个太阳翼帆板;安装在左舱板和碳纤维承力筒上的平台单机;安装在搭载板的搭载区的多个搭载单机;安装在碳纤维承力筒右侧面的高功耗单机;安装在碳纤维承力筒下侧面的分离机构;以及安装在碳纤维承力筒下侧面的推进器。
Satellite platform configuration for carrying services
一种面向搭载业务的卫星平台构型
2024-05-14
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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