The application status of the spacecraft EPS technology researched and developed by Shanghai Academy of Spaceflight Technology ( SAST) during half century in the field of Chinese satellite, spaceship and international satellite was described.

Spacecraft simulation technology is a combined product of system simulation and aerospace engineering, which is a cornerstone of aerospace industry.

航天器仿真技术，是系统仿真与航天工程相结合的产物，是航天事业取得发展的基石。

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The Progress of Shanghai Spacecraft EPS Technology in the 20th Century

20世纪上海航天器电源技术的进展

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The development of spacecraft vacuum technology in China is expected.

展望了中国航天器真空技术的发展。

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But China has also achieved stunning progress with technology breakthroughs in such vital fields as wireless communications, permanent magnetic levitation rail transport, missile and spacecraft technology, and much more.

不过，中国也实现了惊人的进步，它在无线通信、磁悬浮运输、导弹和空间技术等很多重要领域都取得了技术突破。

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The special environment of a spacecraft with electric propulsion and its effects

电推进航天器的特殊环境及其影响

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A Hall thruster, with its high-efficiency and high specific impulse, is one of the most important electric propulsion devices widely used for spacecraft propulsion such as attitude control, orbital transfer and deep space exploration missions in the future.

霍尔推力器作为一种等离子体装置，以其高效率高比冲等特点成为国际电推进领域的研究热点，广泛应用在姿态控制，轨道转移及将来的深空探测任务。

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In particular, the Bond-graph-based method and the Miniature Mode Estimation system can used to detect and isolate faults in spacecraft propulsion system.

针对混合系统的故障检测与诊断问题，本文以推进系统为对象，研究了键图理论和Miniature Mode Estimation方法在其故障检测与隔离中应用与实现方案。

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Based on the physical and mathematical model of spacecraft propulsion system, the application of model based fault diagnosis method to the propulsion system of spacecraft was studied.

在飞船推进系统的物理和数学模型的基础上，研究了基于模型的故障诊断方法在飞船推进系统中的应用。

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By applying the diagnosis method proposed to the spacecraft propulsion systems, the results show that the relation-based fault diagnosis method is effective.

以空间推进系统为研究对象进行了实例诊断分析，结果表明：该方法是一种有效的基于定性模型故障诊断方法。

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Numerical simulation of liquefied gas self-pressurization for small spacecraft propulsion systems

小型航天器液化气推进系统的数值模拟

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Model-based fault diagnosis system for the spacecraft propulsion system

基于模型的航天器推进系统故障诊断

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Dynamic characteristics of priming process in spacecraft propulsion system(ⅰ) theoretical model and simulation results

航天器推进系统管路充填过程动态特性（1）理论模型与仿真结果

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Dynamic Characteristics Study of Spacecraft Propulsion System Engine

航天器推进系统发动机动态特性研究

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Numerical simulation on atomic oxygen action to spacecraft surface material& polyimide in Leo

低地球轨道环境原子氧对航天器表面材料聚酰亚胺作用的数值模拟

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Experimental investigations of the respective and synergistic effects of vacuum ultraviolet radiation and atomic oxygen on a spacecraft material& Kapton

空间材料Kapton的真空紫外与原子氧复合效应研究

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Wind-Induced Response Analysis of Spacecraft-Launching Tower

航天器发射塔风振响应分析

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The article introduces the method of hazard assessment used widely in petroleum and chemical industry, and assesses the hazard of conventional liquid propellant operation in spacecraft launching site by 3 methods.

介绍了在石油化工系统广泛应用的危险评价方法，并利用3种方法对发射场液体推进剂作业进行了危险性评价，初步证明了其在推进剂危险评价中的可行性；

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China's spacecraft launching sites are capable of making both domestic satellite launches and international commercial launches, and carrying out international space cooperation in other fields.

中国航天器发射场既可完成国内发射任务，又具有完成为国际商业发射服务和开展其他国际航天合作的能力。

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The system concept designing methods and procedures for spacecraft launching tower and the basic concepts for different launching processes are briefly described.

简要叙述航天飞行器发射塔总体方案的设计方法和步骤，不同的发射工艺流程可能选择的基本方案。

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Manned spacecraft launching window and solar array optimum sunshine

载人航天器的发射窗口及太阳能帆板的最佳受晒

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