应用结构化分析法开发MIS系统

管理信息系统（ＭＩＳ）的开发应用正在我国企业中兴起，ＭＩＳ的开发方法要科学和规范化，以避免开发工作出现紊乱现象及一些低水平的封闭式的开发。本文介绍了结构化分析法在系统的生命周期中的基本思想和特点，及其在系统分析，总体规划中的一些技术，方法和工具。     

基于空间卫星综合应用系统的天气预报业务框架构建

围绕空间卫星综合应用系统，在介绍天气预报业务系统基本框架的基础上，着重分析了天气预报业务化框架、网络的技术特点，以及天气预报业务的一些技术和方法．     

喷射式气氮调温系统

气氮调温系统是空间环境模拟器中为航天器进行热真空、热平衡试验的关键系统之一。它可使热沉温度在－100℃－＋100℃之间连续可调，并能任意定点。采用喷射式气氮调温系统，与液氮储槽式冷却器调温系统、液氮温度热沉加红外加热笼系统相比，可降低能耗，节约经费。大型空间环境模拟器中由于热沉的热惯性较大以及各支路温度存在均匀性等问题，大型空间模拟器设备要应用喷射式气氮调温系统存在一定难度。KM6大型空间模拟器喷射式气氮调温系统在研制中结合KM6实际和试验要求。调试和使用结果证明这一系统满足试验要求，同时也表明该系统在同一领域达到了国际同类设备的水平。     

空间轨道单粒子翻转率预估方法研究

系统分析了国外单粒子翻转率预估方法，提出了一种适合国内现状的单粒子翻转率预估方法，计算了五个典型轨道上的单粒子翻转率和轨道翻转系数，为评价半导体器件抗单粒子效应的能力提供了依据。     

An experiment to study solar flare effects on radio-communication signals

The occurrence of radio signal fading events caused by ionospheric absorption plays an important role in the performance of radio-communication systems. It is necessary to know the magnitude and time-scale of such events in order to specify technical parameters of the communication system to be used. Generally, fading events are associated with solar flares, which are characterized by sudden increase in the solar X-ray flux that causes an increase in the ionization in the lower ionosphere. The abrupt increase of ionization causes the absorption of radio waves propagating in the Earth–ionosphere wave-guide and is reported as radio signal fading events. A simple experiment to monitor the behavior of lower ionosphere has been carried out at the Southern Space Observatory-SSO/INPE (29.43°S, 53.8°W), located in southern Brazil. The experiment is basically a computer controlled radio receiver that records the received signal strength of Amplitude Modulated (AM) radio signals in the HF (High Frequencies) range. We analyzed data of the 6 MHz beacon signal that has been transmitted by a broadcasting radio station located about 400 km from the observation site. In this work we present initial results of daily variation of the received signal strength and fading events associated with solar flares observed in the 6 MHz signal monitored by the experiment during 2001. X-ray solar flux data from the GOES-8 satellite were used to identify X-ray solar bursts associated with solar flares. Based on the one-year data collected by the experiment, a statistical summary of fading occurrences and their correlation with solar flares, as well as the distributions of time-scales and magnitudes of such events are presented.     

PC—DIO─96接口板在大尺寸计量标准中的应用

介绍了美国NI公司的数据采集板PC—DIO—96的功能,及其在Windows95下软硬件的安装,描述了如何使用其随板软件包,并给出了其三种主要功能（线功能、口功能和组功能）的程序框图。详细介绍了在“建立大尺寸计量标准”题目中应用该板进行环境参数的采集和电机控制。     

乙烯基硅橡胶生胶中低分子的脱除

由于硅橡胶是用催化平衡的方法制备，生胶中含有约3％的挥发性的低分子量环体，会对硅橡胶的热真空失重（TML）、可凝挥发物性能（CVCM）有极大影响。为使所制得的硅橡胶符合空间级材料要求，分别采用溶剂抽提法和热真空处理法来脱除乙烯基硅橡胶中的小分子，通过比较处理前后硅橡胶的分子量及其分布、TML、CVCM，对比了两种方法脱除小分子的效果；并制备得到了符合空间级标准的硅橡胶。     

Ground experimental investigations into an ejected spray cooling system for space closed-loop application

Spray cooling has proved its superior heat transfer performance in removing high heat flux for ground applications.However,the dissipation of vapor–liquid mixture from the heat surface and the closed-loop circulation of the coolant are two challenges in reduced or zero gravity space environments.In this paper,an ejected spray cooling system for space closed-loop application was proposed and the negative pressure in the ejected condenser chamber was applied to sucking the two-phase mixture from the spray chamber.Its ground experimental setup was built and experimental investigations on the smooth circle heat surface with a diameter of 5 mm were conducted with distilled water as the coolant spraying from a nozzle of 0.51 mm orifice diameter at the inlet temperatures of 69.2 °C and 78.2 °C under the conditions of heat flux ranging from 69.76 W/cm~2 to 311.45 W/cm~2,volume flow through the spray nozzle varying from 11.22 L/h to 15.76 L/h.Work performance of the spray nozzle and heat transfer performance of the spray cooling system were analyzed;results show that this ejected spray cooling system has a good heat transfer performance and provides valid foundation for space closed-loop application in the near future.     

航天器对接中接近至首次接触阶段的数值仿真

确定接触点问题是航天器对接过程中接近与接触阶段的仿真的关键问题。以内导向瓣异体同构周边式对接机构为例，给出了确定接触点的方法，建立了确定接触点的数学模型、接近与接触阶段两航天器的刚体运动方程，并对接近与接触阶段进行了数值仿真。仿真结果表明：所建立的数学模型和动力学方程是正确的。     

大型空间环模设备液氮系统冷箱设计

液氮系统是大型空间环境模拟设备中的主要分系统之一,液氮流程采用了单相密闭循环、文丘利管、液氮泵增压及阀门冷箱的结构方案。文章重点介绍了阀门冷箱的设计,这是近年来国外大型空间模拟器液氮流程发展的新趋势。