The invention provides a magnetic levitation platform satellite load expansion heat dissipation surface temperature control device which is characterized by comprising a magnetic levitation platform load (1), an externally-attached heat pipe (2), a heat source (3), a heat dissipation flat plate (4), a cabin plate hole (6) and a solar radiation isolation device (7). Based on the measures of adding a heat dissipation flat plate, externally attaching a heat pipe, a solar radiation isolation device and the like, the heat dissipation efficiency is greatly improved, and the large-power-consumption load heat dissipation problem of the magnetic levitation platform is effectively solved. The device solves the problem of in-orbit heat dissipation of the load space telescope in the solar exploration science and technology test satellite cabin, can also be used for reference for the problem that heat dissipation of large-power-consumption loads of other magnetic levitation platforms is difficult, and has the advantages of being high in adaptability, good in reliability and flexible in design.
本发明提供了一种磁浮平台卫星载荷拓展散热面控温装置,其特征在于,包括:磁浮平台载荷(1)、外贴热管(2)、热源(3)、散热平板(4)、舱板开孔处(6)、太阳辐射隔离装置(7)。本发明基于增加散热平板、外贴热管、太阳辐射隔离装置等措施,极大提高散热效率,有效解决磁浮平台大功耗载荷散热问题。本发明解决了太阳探测科学技术试验卫星舱内载荷空间望远镜在轨热量排散问题,对于其它磁浮平台大功耗载荷难以散热的问题同样可以借鉴使用,具有高适应性、可靠性好、设计灵活的特点。
Magnetic levitation platform satellite load expansion heat dissipation surface temperature control device
磁浮平台卫星载荷拓展散热面控温装置
2023-10-27
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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