The invention discloses a satellite-borne integrated SAR (Synthetic Aperture Radar) satellite platform, belongs to the technical field of spacecrafts, and solves the problems that the temperature uniformity of a mounting plate of an existing satellite platform is poor, the appearance envelope of an SAR antenna is large, the high-precision single-machine mounting requirement cannot be met, and the structural strength is low. The platform comprises an SAR antenna, a feed source assembly, a single machine mounting plate, an out-cabin single machine, an in-cabin single machine, a platform main frame and a solar sail. The platform main frame, the single-machine mounting plate and the solar sail form a cabin body; the solar sail is arranged below the platform main frame; an SAR antenna, a feed source assembly and an outboard single machine are mounted on the outer surface of the single machine mounting plate; an in-cabin single machine is mounted on the inner surface of the single machine mounting plate; the single machine mounting plate comprises a honeycomb plate, a metal gasket and a pre-buried heat pipe; the honeycomb plate comprises a honeycomb core and a honeycomb plate skin; and the metal gasket is connected with the embedded heat pipe. The method is suitable for satellite platform, spacecraft platform, spacecraft configuration and layout design, spacecraft structure thermal control design, spacecraft on-orbit monitoring and SAR satellite on-orbit active compensation.

    一种星载一体化SAR卫星平台,属于航天器技术领域,解决现有的卫星平台安装板温度均匀性差、SAR天线的外形包络大、无法满足高精度单机安装要求及结构强度低问题。本发明平台包括:SAR天线、馈源组件、单机安装板、舱外单机、舱内单机、平台主框架和太阳帆;平台主框架、单机安装板和太阳帆构成舱体;太阳帆设置于平台主框架的下方;单机安装板的外表面上安装SAR天线、馈源组件和舱外单机;单机安装板的内表面上安装舱内单机;单机安装板包括蜂窝板、金属垫片和预埋热管;蜂窝板包括蜂窝芯子和蜂窝板蒙皮;金属垫片与预埋热管相接。本发明适用于卫星平台航天器平台、航天器构型及布局设计、航天器结构热控设计、航天器在轨监测和SAR卫星在轨主动补偿。


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    Title :

    Satellite-borne integrated SAR satellite platform


    Additional title:

    一种星载一体化SAR卫星平台


    Contributors:
    CHEN JIAN (author) / GUO JINSHENG (author) / CHANG HAO (author) / LI ASIHAN (author) / ZHAO CHUNHUI (author) / GUAN ZHILIN (author)

    Publication date :

    2023-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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