The embodiment of the invention provides a nuclear power spacecraft using a modularized shielding body structure, which is characterized in that the spacecraft comprises a reactor (1), a shielding body frame supporting cabin (2), a supporting cabin net cover (3), an unfolding mechanism support (4), a spacecraft solar cell panel (5) and a spacecraft platform instrument equipment cabin (6), wherein the reactor (1) is arranged at one end of the spacecraft, and a shielding body assembly is located between the reactor (1) and the unfolding mechanism (4); the reactor and a spacecraft platform are separated by the unfolding mechanism (4), and the spacecraft platform is located on the other side farthest from the reactor and comprises the spaceflight instrument and equipment cabin (6) and the spacecraft solar panel (5).

    本发明实施例提供了一种使用模块化屏蔽体结构的核动力航天器,其特征在于,所述航天器包括:反应堆(1),屏蔽体框架支撑舱(2)、支撑舱网罩(3)及展开机构支撑(4)、航天器太阳能电池帆板(5)以及航天器平台仪器设备舱(6);其中,所述反应堆(1)在航天器的一端,所述屏蔽体组件位于所述反应堆(1)与展开机构(4)之间;展开机构(4)将反应堆与航天器平台分隔开开,航天器平台位于与反应堆相距最远的另一侧,包括航天仪器设备舱(6)、太阳能帆板(5)。


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    Title :

    Nuclear power spacecraft using modularized shielding body structure


    Additional title:

    一种使用模块化屏蔽体结构的核动力航天器


    Contributors:
    MENG TAO (author) / KANG ZHIYU (author) / YANG YANLEI (author) / ZHU JUNJIE (author) / WANG ZHONGYUAN (author) / XIA CHENCHAO (author) / WANG ZHAO (author) / TANG SHENGYONG (author) / LUO CHAO (author) / XU TAO (author)

    Publication date :

    2022-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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