... 航天器结构系统structural system of spacecraft 航天器热控系统spacecraft thermal control system 航天器设计、制造与试验design, manufacture and test of spacecraft ...
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The results indicate that the mini thermoelectric heat pump-PCM thermal control system can provide effective thermal control of high power spacecraft electronics.
结果表明，采用该热控系统对航天器短时大功率组件进行温度控制是可行的。
Objective To deal with the mass optimization of thermal control system as well as environmental control and life support system(ECLSS) of manned spacecraft.
目的解决载人航天器热控和环控生保系统的轻量化问题。
A novel heat pump ice thermal storage integration scheme based on reducing total mass (including relative power system mass) of thermal control system of spacecraft is presented.
提出了旨在降低热控系统质量的热泵-蓄冷组合热控方案。
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