蒸汽压缩热泵是未来大型航天器热控系统和制冷设备的新方案。
Vapor compression heat pump is a new concept of thermal control system and refrigerator for future space use.
结果表明此主动热控系统能对航天器电子设备温度进行有效控制。
The result shows that this system with fuzzy control could control the electronics temperature effectively.
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。
The results indicate that the mini thermoelectric heat pump-PCM thermal control system can provide effective thermal control of high power spacecraft electronics.
目的解决载人航天器热控和环控生保系统的轻量化问题。
Objective To deal with the mass optimization of thermal control system as well as environmental control and life support system(ECLSS) of manned spacecraft.
在保证航天器废热排放量的基础上，通过计算对比分析了固定转速热泵回路热控系统和变速热泵回路热控系统的耗电量，结果证明后者比前者节能20%左右。
The power consumption of variable speed heat pump loop and fixed speed heat pump loop are compared through calculation, on the basis that the spacecraft has the same heat load.
在保证航天器废热排放量的基础上，通过计算对比分析了固定转速热泵回路热控系统和变速热泵回路热控系统的耗电量，结果证明后者比前者节能20%左右。
The power consumption of variable speed heat pump loop and fixed speed heat pump loop are compared through calculation, on the basis that the spacecraft has the same heat load.
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