Space radiator is an important component in spacecraft thermal control subsystem.
在航天器热控制中，空间辐射器是最主要的排热部件。
Space radiators are important components in spacecraft thermal control subsystem.
大多数航天器的热控制都是利用空间辐射器作为排热部件。
Glass partitions are framed in aluminum and have double glazing for thermal control.
玻璃分区被铝条分割成框架，同时还运用了双层玻璃的热控制系统。
Thermal control is much easier in solution polymerization compared to bulk polymerization.
与本体聚合相比，在溶液聚合中对反应热的控制比较容易。
The paper provides valuable guidance to improving the thermal control and thermal deformation of PAA.
本文所完成的工作对相控阵天线的热控制及热变形研究具有一定的指导意义。
Vriable emittance thermal control device is one of the focus of the future spacecraft thermal control.
可变发射率热控器件是未来航天器热控的焦点之一。
The suggestions are put forward about the reliability research of thermal control system in the future.
对今后关于热控系统可靠性的研究提出了建议。
Vapor compression heat pump is a new concept of thermal control system and refrigerator for future space use.
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。
Some operation modes of the porous plate water sublimator used in an EVA space suit thermal control system are discussed.
对舱外航天服热控系统所采用的多孔板水升华器的主要工作模式进行了讨论。
This article details the rapid thermal control system for home electric water heater hardware circuit and software design.
本文详细叙述了快热式家用电热水器控制系统硬件电路和软件的设计。
Thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system.
单组元肼分解发动机的热控制与热分析是空间推进系统重要组成部分。
Well-deployed natural features can improve water management and thermal control and reduce operating costs, but they are not a panacea.
精心部署的自然特征能提高水管理和热控制并降低操作成本，但它们并不是包治百病的万能药。
The existing problems and retrofitting measures of thermal control equipment of 300MW unit in Fengcheng power plant are elaborated.
阐述了丰城电厂30 0MW机组热控设备存在的问题及采取的改造措施。
Through analyzing and application, the design and tuning methods of big capacity fire power plant thermal control system are concluding.
通过分析与应用总结出适用于大型火力发电厂热力控制系统的设计、调整方法、手段，并在工程应用中得到实践。
The research results have referenced values for the evaluation of working reliability and the thermal control design and implementation.
研究结果对丝杠副工作热可靠性评估、机构热控方案的设计和实施有实际参考价值。
After analyzing the thermal environment of Windows, related active and passive thermal control way and its work principle are introduced.
在对窗口热交换过程进行具体分析后，介绍了针对各漏热环节所采取的主动热控和被动热控措施及其工作原理。
Experimental results showed that the properties of two coatings were stable and they reached the requirements of the thermal control design.
实验结果表明，涂层性能稳定并达到了热控设计的要求。
The calculations of radiator surface area and heat insulation layer thickness are necessary for the design of passive thermal control system.
纳卫星的被动热控系统对卫星舱内的温度控制及其有效载荷的可靠工作具有重要意义。
Thermal control material OSR's have to meet a variety of ground and space environments during ground storage and space flight of space vehicles.
航天器在地面待发射期间加空间实际飞行过程中，热控元件OSR要遇到各种地面和空间环境。
First step of the method is to set up math model of thermal control system and store the results of computation into the computer fault database;
该策略是基于热控系统数学模型建立故障诊断数据库；
It is difficult for reverse load control algorithm to balance the system throughput and rise-over-thermal control in the CDMA EVDO data systems, which.
针对数据系统，负荷控制算法的难点在于反向链路数据的突发性对系统造成的干扰，以及如何平衡系统吞吐量与抑制反向干扰。
The platform is applied to documents designing of satellite thermal control system successfully. It improves work efficiency and standardization greatly.
该平台成功应用于卫星热控系统的文档设计，极大地提高了设计工作的时效性和规范性。
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。
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。
It is concluded from the paper that, the humidity control technique used by the thermal control system is successful, and ensure the full success of the (satellite's) task.
通过研究可得，热控系统所采取的卫星湿度控制技术是成功的，保证了卫星任务的圆满完成。
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。
Phase change thermal control has been widely used in thermal control of electronic devices recently because it has compact structure, reliable performance and energy-saving property.
相变温控因其装置结构紧凑、性能可靠、经济节能等优点近年来被广泛地应用在各类电子设备的温控上。
The research meaning of this subject is to find out the most suitable method of design of controller witch has good robust stability and witch is suitable for thermal control target .
这一课题的研究意义就在于，在理论分析及仿真试验的基础上找出最为适合热工控制对象参数时变这一特性的具有较强鲁棒性的控制器设计方案。
Base on the theory of differential thermal expansion between the two materials having different CTE values, a thermal switch as a crucial part in the thermal control system is designed.
根据具有不同温度膨胀系数的材料遇热变形不同的原理，设计了该热控系统的关键部件-热开关。
Base on the theory of differential thermal expansion between the two materials having different CTE values, a thermal switch as a crucial part in the thermal control system is designed.
根据具有不同温度膨胀系数的材料遇热变形不同的原理，设计了该热控系统的关键部件-热开关。
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