The invention relates to a moonlet platform and load integrated configuration, and belongs to the field of satellite platform configuration design. Comprising a space camera, a bearing cylinder, a satellite-rocket adapter, an equipment mounting structural plate, two satellite solar wings and three star sensors, wherein the bearing cylinder is vertically arranged in the axial direction; the outer side of the bearing cylinder is sleeved with the equipment mounting structural plate; through holes are formed in the upper and lower ends of the equipment mounting structural plate, so that the upper and lower ends of the bearing cylinder are exposed from the equipment mounting structural plate; the satellite-rocket adapter is coaxially mounted at the bottom of the bearing cylinder; the space camera is coaxially mounted at the top of the bearing cylinder; the three star sensors are uniformly arranged on the outer wall of the space camera along the circumferential direction; the two satellite solar wings are symmetrically arranged on the two sides of the bearing cylinder; according to the invention, the satellite meets the design requirements of small satellite mass, small size, small mass characteristic, high agility maneuverability and high imaging quality.
本发明涉及一种小卫星平台与载荷一体化构型,属于卫星平台构型设计领域;包括空间相机、承力筒、星箭适配器、设备安装结构板、2个卫星太阳翼和3个星敏感器;其中,承力筒轴向竖直放置;设备安装结构板套装在承力筒的外侧;设备安装结构板的上下两端设置有通孔,实现承力筒的上下两端从设备安装结构板露出;星箭适配器同轴安装在承力筒的底部;空间相机同轴安装在承力筒的顶部;3个星敏感器沿周向均匀设置在空间相机的外壁;2个卫星太阳翼对称设置在承力筒的两侧;本发明使卫星满足卫星质量小、体积小、质量特性小和敏捷机动性强、成像质量高的设计要求。
Small satellite platform and load integrated configuration
一种小卫星平台与载荷一体化构型
2023-06-02
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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