氙离子发动机对GEO卫星表面充/放电效应的影响

用于GEO卫星上的氙离子发动机工作时喷射出具有一定能量和密度的氙离子及电子,参与了通常由空间等离子体、表面材料二次电子、光生电子等对GEO卫星的表面充/放电过程,从而对卫星表面充/放电效应产生影响。文章对此影响进行定性分析,并探讨其设计要求。     

遮挡板参数对二元喷管气动和红外辐射影响

采用计算流体力学/红外辐射强度数值计算的方法,以宽高比3.33二元收敛喷管为研究对象,计算分析了二元喷管加双层遮挡板结构对喷管气动和红外辐射影响.结果表明:二元喷管加遮挡板后,总压恢复系数系数和推力系数并未降低,在98.81％和95.15％以上;单层遮挡结构的二元喷管在绝大多数角度都比基准二元喷管高,且增加的幅度较大;与基准二元喷管相比较,双层遮挡板结构的喷管在-90°至-10°探测方向上红外辐射强度降低38％-80％,但是由于上遮挡板的存在,喷管上方(30°-90°)的红外辐射增强;遮挡间距增加,引射气流流量增加,上、下遮挡板红外辐射减小,当遮挡间距增加到35mm时,上遮挡板的红外辐射峰值降低到800W/Sr,下遮挡板红外辐射强度仅为4W/Sr左右.这说明了双层遮挡结构的二元喷管(喷口后延)在某些方向上有较强的红外抑制效果.     

Molecular Hydrogen

Observations of H₂ line emission in galactic and extragalactic environments obtained with the Infrared Space Observatory (ISO) are reviewed. The diagnostic capability of H₂ observations is illustrated. We discuss what one has learned about such diverse astrophysical sources as photon-dominated regions, shocks, young stellar objects, planetary nebulae and starburst galaxies from ISO observations of H₂ emission. In this context, we emphasise use of measured H₂ line intensities to infer important physical quantities such as the gas temperature, gas density and radiation field and we discuss the different possible excitation mechanisms of H₂. We also briefly consider future prospects for observation of H₂ from space and from the ground. Based on observations with ISO, an ESA project with instruments funded by ESA Member States (especially the PI countries: France, Germany, The Netherlands, and the United Kingdom), and with the participation of ISAS and NASA.     

环境电离辐射体源标准空气比释动能率的确定

介绍了用实测法和MC理论计算法确定"放射性模型体源"表面中心点上方不同高度的比释动能率的方法和研究成果.研究结果表明,实测和理论计算结果的一致性较好,不存在明显的系统差.由此首次拟合出了能客观反映我国环境电离辐射体源标准的单位核素含量空气比释动能率的贝可法换算系数,提高了采用贝可法确定模型体源空气比释动能率的准确度.     

On the Lyman α and O VI Line Profiles in Streamers and Coronal Holes

The profiles of the Lyα line at 1215.6 Å and of the O VI doublet at 1031.9 Å and 1037.6 Å in the extended solar corona have been analyzed vs. latitude and radial direction, performing observations with the Ultraviolet Coronagraph Spectrometer (UVCS) on board the ESA-NASA solar satellite SOHO (Solar and Heliospheric Observatory). The results show that these lines behave differently with latitude: the H I Ly α line has larger full width at half maximum (FWHM) values in the streamer region and narrower values towards the pole, while the FWHM of O VI lines has a minimum at the center of the streamer and slightly increases towards the polar regions. We briefly discuss the impact of the results on coronal heating theories.     

强驻波声场对微小颗粒群作用的实验研究

用实验手段研究了以空气为介质的强驻波声场 (声压级大于 1 5 0dB)对其中微小颗粒群 (颗粒直径小于 30 μm)的作用。实验中观察到了颗粒有规律地向波节点运动的现象 ,并发现聚集颗粒群中含有周期性长大、破裂而喷发的气泡。这些现象与声流及声辐射压力有关。对这些现象的观察和分析有助于加深对高声强下一些基本效应的认识     

边界层综合诊断技术研究

给出了对二元翼型模型和三元三角翼模型表面边界层转捩用表面热膜技术、红外热像仪技术和液晶显示技术在同一风洞中同时进行显示和测量并进行比较的结果。对二元NACA-0012翼型表面边界层转捩点位置测量，三种方法都给出了相吻合的结果。三元的60°三角翼模型经过多次实验，测量结果表明表面热膜技术能够给出三角翼模型表面边界层转捩位置的定量侧量结果。红外热像仪技术和液晶显示技术研究在应用时受到环境条件的影响，在合适的条件下也能给出模型表面边界层转捩位置的定量结果。     

F3H红外定标试验用空间环模设备

F3H为星载遥感光学仪器红外通道标定和红外系统性能测试专用的空间环模设备。设备主要包括:真空容器系统、真空抽气系统、氮系统、氦气制冷系统、数据采集系统、试验管理系统等。启动氦气流程后,尺寸为2.5m×1m的冷屏的温度可以降至18K以下,真空容器内可获得优于4×10-6Pa的超高真空。该冷屏是目前国内最大的冷屏,可以供4台光学遥感仪器同时进行红外定标试验。通过试验证明,设备各系统性能稳定,运行正常,达到设计指标要求。     

电动密集架控制技术的研究

本文主要研究了计算机网络控制电动密集架的动力系统、安全保护措施和数据库管理的功能特点。     

Understanding Galaxy Formation with ISO Deep Surveys

We present the results obtained through the various ISO extragalactic deep surveys. Although IRAS revealed the existence of galaxies forming stars at a rate of a few tens (LIRGs) or even hundreds (ULIRGs) solar masses in the local universe, ISO not only discovered that these galaxies were already in place at redshift one, but also that they are not the extreme objects that we once believed them to be. Instead they appear to play a dominant role in shaping present-day galaxies as reflected by their role in the cosmic history of star formation and in producing the cosmic infrared background detected by the COBE satellite in the far infrared to sub-millimeter range. Based on observations with ISO, an ESA project with instruments funded by ESA Member States (especially the PI countries: France, Germany, The Netherlands, and the United Kingdom), and with the participation of ISAS and NASA.