星载极化散射计系统设计研究

文章介绍了星载极化散射计的研究背景、意义、概念及特点,在此基础上,讨论了系统设计时的系统体制、极化方式、隔离度等问题,提出了一种星载极化散射计系统设计的初步方案构想。     

先进的电子战测试设备(AEWTS)能满足通用测试要求

由豪涅威尔公司研制的先进电子战测试设备(AEWTS)称为测试站。这个系统的结构布局极好,并有满足将来通用的测试要求的灵活性。高性能总线和硬件、软件的模块化有助于测试站的扩充,但是测试站要扩充的话还必须增加更多的资源。先进电子战测试设备从1970年末开始发展到目前这种颇有活力的状况,充分说明了该系统的潜在的扩展能力以及它的自适应性。     

在(工作)持续时间短暂设备中伴随有燃烧的气体动力模型试验方法的特点

对在高焓、持续工作时间短暂设备中进行伴有燃烧过程的气体动力模型的试验方法的特点作了介绍。根据俄罗斯科学院西伯利亚分院理论及应用研究所组织这种试验工作所积累的经验 ,描述了解决各种各类与燃烧有关的问题的模型配备 ;在发动机进气道中的推力空气动力特性、压力及热通量的测量结果等等。由此说明试验时间为 50～ 2 0 0ms的热射式风洞是解决燃烧问题的可靠设备     

Laser Hardening of Metals

The first experiments on hardening metals by laserpeening induced residual compressive stress in the sur-face of metals for improving their resistance to cracking,stress corrosion and fatigue took place more than 30years ago. However, only today, with the development ofhigh-intensity pulse repetitive rate lasers, this methodstarts to compete to traditional peening, which use influ-ence of small metal balls.Laser peening uses pulses with high intensity 109￣1010 W/cm2 [1]. The laser energy abso…     

CDAS 主站测距机方案设计

为完成风云二号卫星三点测距任务,研制了ＣＤＡＳ主站测距机。介绍了测距机的用途和功能,叙述了侧音测距原理和距离测量过程,给出了测距机性能指标和系统组成,设计了一纯侧音测距体制的测距机方案,讨论了方案设计的技术特点及其达到的性能。     

行星际磁场的螺旋扇形过渡区

从行星际磁场的大尺度螺旋形构型和扇形边界附近太阳风流动与冕旒的可能相关,本文得到一个推论,即在行星际空间可能存在一种较厚的螺旋扇形过渡区。行星际磁场和太阳风的实地观测证实了这种较厚的螺旋扇形过渡区的存在。在所分析的45个螺旋扇形过渡区中,磁场强度都不为零;大部分大于或小于周围平均场强。本文进一步分析了磁增大和磁减小两类过渡区中的物理性质和可能成因。      

Science Missions Using CubeSats

As the role of missions and experiments carried out in outer space becomes more and more essential in our understanding of many earthly problems, such as resource management, environmental problems, and disaster management, as well as space science questions, thanks to their lower cost and faster development process CubeSats can benefit humanity and therefore, young scientists and engineers have been motivated to research and develop new CubeSat missions. Not very long after their inception, CubeSats have evolved to become accepted platforms for scientific and commercial applications. The last couple of years showed that they are a feasible tool for conducting scientific experiments, not only in the Earth orbit but also in the interplanetary space. For many countries, a CubeSat mission could prompt the community and young teams around the world to build the national capacity to launch and operate national space missions. This paper presents an overview of the key scientific and engineering gateways opened up to the younger scientific community by the advent and adaptation of new technology into CubeSat missions. The role of cooperation and the opportunities for capacity-building and education are also explored. Thus, the present article also aims to provide useful recommendations to scientists, early-career researchers, engineers, students, and anyone who intends to explore the potential and opportunities offered by CubeSats and CubeSats-based missions.      

四向增强碳-碳复合材料的研究

四向织物增强碳一碳复合材料的研究工作正在进行中。这种复合材料是为制造在工作时承受很高的热应力的零、部件而专门设计的。本文概要地描述了四向织物并指出它与三向、七向、十一向相比较所具有的优点。四向织物是用单向碳纱按“抽拉工艺”制得的杆制造的,复合研究证明沥青在压力下浸渍-碳化工艺是优越的。     

铝锂合金——新一代轻型金属结构材料

在低比重铝合金基础上发展起来的铝锂合金的进展愈来愈快,在此期间首先为商业的需要,制造出了半成品,并投放市场。本文介绍了为首的三名制造者Alcan,Alcoa及Pechiney制造的合金,并说明了目前铝锂合金的研究和发展状况,同时试图谈谈未来发展概况。     

双三角翼局歼击教练飞机的概念优化设计

双三角翼气动布局比三角翼飞机具有更好的大攻角空气动力特性。引入了评估教练机训练效能的作战分析法，研究了双三角机翼布局飞机空气动力特性的工程计算途径以及飞机性能指标的确定方法。以训练效能作为目标函数并选取机翼平面形状的几何参数为设计变量，采用多变量数值寻优方法，在战术技术指标及相关几何约束条件下，对某高级教练机的双三角机翼气动布局方案进行了优化选择。算例表明最优方案不仅比原准方案具有更高的训练效能，还改善了结构的受力情况，与工程实践吻合。