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.
主要叙述通信用大功率半导体激光器温控原理及激光组件的构成。
The principle of temperature control of high power semiconductor laser for communication and the composition of laser module are described.
在3d - MCM(多芯片组件)封装设计中，大功率和高热流密度导致系统的散热成为关键技术之一。
In 3d-mcm (multi chip module) packaging designs, heat dissipation is one of the key issues that must be solved.
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