Thermal Design and On-Orbit Thermal Analysis of 6U Nano-Satellite High Resolution Video and Image (HiREV)

Han-Seop Shin, Hae-Dong Kim
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Abstract

Korea Aerospace Research Institute has developed 6U Nano-Satellite high resolution video and image (HiREV) for the purpose of developing core technology for deep space exploration. The 6U HiREV Nano-Satellite has a mission of high-resolution image and video for earth observation, and the thermal pointing error between the lens and the camera module can occur due to the high temperature in camera module on mission mode. The thermal pointing error has a large effect on the resolution, so thermal design should solve it because the HiREV optical camera is developed based on commercial products that are the industrial level. So, when it operates in space, the thermal design is needed, because it has the best performance at room temperature. In this paper, three passive thermal designs were performed for the camera mission payload, and the thermal design was proved to be effective by performing on-orbit thermal analysis.
6U纳米卫星高分辨率视频图像(HiREV)热设计与在轨热分析
韩国航空宇宙研究院为开发深空探测核心技术,开发了6U纳米卫星高分辨率影像(HiREV)。6U HiREV纳米卫星具有对地观测高分辨率图像和视频的任务,在任务模式下,由于相机模块温度较高,会导致镜头与相机模块之间的热指向误差。HiREV光学相机是基于工业级的商业产品开发的,热指向误差对分辨率影响较大,因此热设计应解决这一问题。因此,当它在太空中运行时,需要进行热设计,因为它在室温下具有最佳性能。本文针对相机任务载荷进行了三种被动热设计,并通过在轨热分析验证了热设计的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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