航天器热控制

在航天器热控制中，空间辐射器是最主要的散热部件。

Space radiators are important components in spacecraft thermal control subsystem .

首先全面论述了航天器热控制和热分析的基本内容，指出本课题产生的工程背景。

Firstly , there is a full discuss of space aircraft thermal control .

铝光亮阳极氧化涂层是一种重要的航天器热控制材料。

The white anodic film on aluminium surface is a kind of important thermal control coatings for spacecraft .

空间辐射器作为航天器热控制中的重要散热部件，是航天器与太空环境进行热量交换的主要装置，是航天器排热系统的重要组成部分。

As an important heat dissipating system in spacecrafts , the radiator is the main heat-exchanging device between the spacecraft and the outer space ; therefore it forms one of those most important components in the spacecraft .

空间热泵排热系统由于能够利用循环工质的潜热，提高辐射器的工作温度，提升废热的品质，性能系数高，因而被广泛认为是下一代航天器热控制技术。

Heat pump system is widely considered as the next generation thermal control technology of spacecraft because of being able to take advantage of the refrigerant latent heat , raising radiator temperature , improving the quality of waste heat and having a higher COP .

航天器主动热控制系统辐射散热的半物理仿真

Semi-physical Simulation of Radiation for Active Thermal Control System of Spacecraft

航天器热控和环境控制生命保障系统热网的优化

Optimization of thermal network for spacecraft thermal control and environment control and life support system

为了减小载人航天器热控和环境控制生命保障系统的质量，在建立的单回路和内外耦合回路流动换热和质量构成的物理数学模型基础上，对系统进行了全局轻量化的计算和分析。

Global optimization of the governing equations for the flow and the heat and mass transfer in single loop and dual loop systems was used to reduce the mass of a spacecraft thermal control system and the environmental control and life support system .