The invention provides a deep space exploration spacecraft. The spacecraft is divided into three parts, namely an instrument cabin, a load cabin and a supporting cabin. The supporting cabin is used for bearing the landing detector and separating the landing detector when reaching a preset orbit, so that the landing detector lands to an outer planet for landing detection; the load cabins are independently designed and arranged in the supporting cabin and the instrument cabin, large-size detection loads are installed on the load cabins, space coupling of the large loads and the main platform is reduced, and the adaptability of the spacecraft to the geometrical shape and weight of the large loads is improved. The instrument cabin is a main body of the spacecraft, in a limited space, besides GNC, propulsion, integrated electronics, measurement and control systems and the like of a conventional spacecraft, various scientific detection effective loads are further arranged to carry out long-term scientific detection on an external planet, and earth data transmission equipment is arranged to download detection data in real time; and the layout self-monitoring equipment can obtain mechanism actions and body pictures on the spacecraft in real time.
本发明提供了提供一种深空探测航天器。所述航天器分为三部分,仪器舱、载荷舱和支撑舱。支撑舱用于承载着陆探测器,到达预定轨道将着陆探测器分离,使其着陆到外星球进行着陆探测;载荷舱独立设计,布置在支撑舱、仪器舱内部,其上安装大尺寸探测载荷,减小大载荷与主平台的空间耦合,提高航天器对大载荷几何形状和重量的适应性。仪器舱是航天器的主体,在有限的空间下,除布置常规航天器的GNC、推进、综合电子、测控等系统外,还布局多种科学探测有效载荷对外星球进行长期科学探测,布局对地数传设备将探测数据实时下传,布局自监视设备可实时获取航天器上机构动作和本体画面。
Deep space exploration spacecraft
一种深空探测航天器
03.05.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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