A multi-stage buffer heat suppression structure for a high-orbit space telescope is characterized in that through a shielding layer coating design of a telescope main body structure and a light inlet structure, sunlight is isolated from entering a light inlet by utilizing multi-stage heat insulation and temperature control, thermal disturbance of multi-layer heat leakage to the telescope is greatly suppressed, and the problem that the high-orbit space telescope is influenced by sunlight is solved; the high-temperature stability requirement of the telescope is met from the system angle, the temperature stability of the lens assembly reaches the standard, and the detection requirement of gravitational wave weak signals is met.

    一种用于高轨空间望远镜的多级缓冲抑热结构,通过对望远镜主体结构及入光口结构的屏蔽层包覆设计,利用多级隔热及控温,隔离太阳光进入入光口,同时大幅抑制多层漏热对望远镜的热扰动,解决高轨空间望远镜受太阳光的影响,从系统角度实现望远镜高温度稳定性需求,实现镜头组件温度稳定性达标,满足引力波微弱信号的探测需求。


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    Titel :

    Multi-stage buffer heat suppression structure for high-orbit space telescope


    Weitere Titelangaben:

    一种用于高轨空间望远镜的多级缓冲抑热结构


    Beteiligte:
    XIA CHENHUI (Autor:in) / YU FENG (Autor:in) / ZHAO YU (Autor:in) / YANG TAO (Autor:in) / SONG XINYANG (Autor:in) / LU PAN (Autor:in) / ZHANG JIONG (Autor:in) / GUO NAN (Autor:in) / ZHAO HUI (Autor:in) / YANG MING (Autor:in)

    Erscheinungsdatum :

    29.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G02B Optische Elemente, Systeme oder Geräte , OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS / B64G Raumfahrt , COSMONAUTICS



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