美国导弹防御系统的支持技术计划

介绍了美国导弹防御系统支持技术计划中的一些重点项目:助推段拦截计划,先进探测器技术计划和先进拦截弹材料与系统技术计划,通过分析得到了一些有益的启示。     

制导导弹试验仿真中的目标模拟技术

介绍了制导导弹试验仿真中采用的典型目标模拟技术和目前的发展状况,这些目标模拟技术主要包括:信号直接注入技术和目标影像投影技术。详细介绍了几种目标模拟技术的优缺点以及未来的发展趋向。     

卫星激光防护技术

从两方面探讨轨道卫星激光防护技术.介绍卫星光电探测器激光防护设计原理及新型防护技术.对提高卫星结构材料的抗激光损伤能力提出几种实用方法.     

铝合金-纯铝-钢复合板爆炸焊接试验及性能研究

通过设计爆炸焊接试验复合了铝合金-纯铝-钢爆炸复合板,对其界面形态、显微硬度及力学性能进行了研究。结果表明,铝合金-纯铝界面纯规则正弦波形,纯铝-钢复合板界面波形较小,铝合金-纯铝-钢复合板的界面剪切强度在75 MPa以上,爆炸复合过程中,纯铝与钢界面生成了金属间化合物,其界面处基体金属发生强烈的塑性变形。复合板变形及组织变化的结果造成复合板界面处的显微硬度最高,随着距界面距离的增加,两侧基体金属的硬度逐渐降低。     

小口径炮激光模拟器光束传输特性的研究

本文采用多横模振荡模型,对小口径炮激光模拟器光束传输特性进行了分析,导出了射程及光斑大小与激光功率、探测器阈值辐照度、光学系统及大气衰减的关系。并根据现有条件用计算机进行了计算,给出了激光传输过程中光斑分布的理论曲线。在此基础上进行了实地测量,实验值与理论曲线基本吻合。本文对激光模拟器的研制和应用具有一定的参考价值。     

激光模拟器的模匹配

本文根据椭圆高斯模的传输和变换理论,分析了椭圆高斯模的模式变换,讨论了模式匹配的计算,并列举了两种椭圆高斯模的计算实例。     

多波段隐身兼容中的几个矛盾问题的分析

多波段隐身兼容是隐身技术发展的方向,但是每增加一个隐身内容或波段,都对隐身兼容的实现增加很大的难度。分析了多波段隐身兼容技术中存在的几个矛盾问题,包括1 06μm激光隐身与近红外隐身兼容的矛盾、主被动毫米波隐身兼容的矛盾、10 6μm激光与8～14μm热红外隐身兼容的矛盾,同时探讨了解决这些矛盾问题的方法。     

Hyperspectral imaging and remote trace detection of cis-1,3,4,6-tetranitrooctahydroimidazo-[4,5 d] imidazole (BCHMX) compared with traditional explosives using laser induced fluorescence

cis-1,3,4,6-Tetranitrooctahydroimidazo-[4,5 d] imidazole (BCHMX) is an advanced energetic compound that expected to spread worldwide in the near future. Since, no approved remote detection methods were reported in current literature for this material, we performed hyper-spectral imaging and laser induced fluorescence (LIF) to a BCHMX sample under low laser fluence for determining the optimum laser wavelength used in any future BCHMX-LIF based remote detection systems. For this purpose, an experimental setup consisted of a sun spectrum lamp and hyper-spectral camera was built to illuminate and image white powder samples of BCHMX in comparison with the traditional explosives, HMX (1,3,5,7-tetranitro-1,3,5,7-tetraazacyclooctane), RDX (1,3,5-trinitro-1,3,5-triazacyclohexane), PETN (2,2-Bis[(nitroxy)methyl]propane-1,3-diyldinitrate). The imaging reveals strong BCHMX sample absorption contrast among other samples at wavelength ranging from 400 to 410 nm. When light source was replaced by a 405 nm laser diode illuminator, a strong BCHMX sample LIF at the spectral range from 425 to 700 nm was observed under low laser fluence condition of 0.1 mJ/cm². Finally, we demonstrated successfully the ability of the 405 nm LIF and the hyperspectral imaging technique to detect finger print traces of BCHMX on white cellulose fabric from a distance of 15 m and a detection limit of 1 μg/cm².     

Impact of atmospheric turbulence on coherent beam combining for laser weapon systems

The performance of a laser weapon system based on coherent beam combining (CBC) depends on its propagation properties in the atmosphere. In this study, an analytical model based on partial coherent beam combining (PCBC) for assumed coherence coefficients between beams in a CBC lattice was developed. The Kolmogorov model of atmospheric turbulence and the Hufnagel-Valley model of Cn2 dependence on atmospheric parameters were implemented. Novel simplified metrics were proposed to assess the CBC performance. Several beam profiles (super-Gaussian, truncated Gaussian, etc.) and ge-ometries were analyzed in terms of maximal intensity in the far field. An approximate formula for PCBC efficiency dependent on the Fried radius was proposed. The results of CBC modeling were compared to those of the Gaussian beam propagation model in a turbulent atmosphere. The dependence of CBC performance on the Cn2 parameter, range, and elevation angle was analyzed. It could be concluded that the application of CBC for medium and long range propagation is impractical without an effective adaptive optics system.     

Damage to aircraft composite structures caused by directed energy system: A literature review

This paper presents a comprehensive review of the research studies on direct energy system effect on aircraft composite structures to develop a good understanding of state-of-the-art research and devel-opment in this area. The review begins with the application of composite materials in the aircraft structures and highlights their particular areas of application and limitations. An overview of directed energy system is given. Some of the commonly used systems in this category are discussed and the working principles of laser energy systems are described. The experimental and numerical studies re-ported regarding the aircraft composite structures subject to the effect of directed energy systems, especially the laser systems are reviewed in detail. In particularly, the general effects of laser systems and the relevant damage mechanisms against the composite structures are reported. The review draws attention to the recent research and findings in this field and is expected to guide engineers/researchers in future theoretical, numerical, and experimental studies.