本文主要研究了星载TR组件结构设计，热控技术和抗辐照技术三个方面的内容。
This article mainly studies three aspects which are the structure design of space-borne tr module, heat control and anti-irradiation technology.
相同类型组件之间的流量分配是均匀的，已满足热工水力设计要求；
The flow distribution factors among the same type assemblies are almost same, that has satisfied the demand of thermal-hydraulic design;
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