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971.
随着载人航天、深空探测等航天任务的蓬勃发展,航天器回收载荷质量大幅提高,以单具降落伞为功能核心的传统减速系统已不能满足大质量回收载荷日益提高的迫切要求,发展群伞减速着陆系统是实现大载重航天器高效减速和无损着陆要求的发展方向。本文采用数值模拟手段对群伞系统的气动特性开展仿真研究,结合环帆伞构型优化设计,分析了多种构型下群伞系统的气动特性。通过对仿真结果进行流场分析和数据对比发现,开窗/开缝设计既能够确保群伞系统具有良好的阻力特性,又能够维持群伞系统的工作稳定性,避免单伞之间由于受力而发生碰撞现象。采用数值仿真手段不仅可以提高降落伞研制效率,降低研发成本,也为设计人员掌握群伞系统的工作原理、促进降落伞设计理论发展提供了有力保证。  相似文献   
972.
《防务技术》2022,18(11):2034-2044
As an essential component of ammunition, pyrotechnics can control ignition with high reliability. However, due to limits of fabrication technology, traditional pyrotechnics are bulky. To achieve both functionality and miniaturization, MEMS pyrotechnics integrate initiator, safety-and-arming (S&A) device and lead charge and keep all components within a small size. MEMS S&A devices, as the core component to ensure system safety, are difficult to achieve active and rapid response to control signals with high safety and reliability. In order to overcome the difficulty, we propose the design and characterization of a MEMS pyrotechnic with a double-layer barrier S&A device. The MEMS pyrotechnic is a high-integrated device with an overall size of 13.4 × 8.5 × 5.2 mm3. The initiator is a NiCr bridge foil covered with an Al/CuO energetic film, which can generate flame when ignited by an excitation voltage. To match the flame energy, lead styphnate is chosen in this study as the lead charge. The S&A device contains four semi-circular barriers, which are directly driven by V-shape electro-thermal actuators to gain active control of the pyrotechnics' ignition condition with rapid response. To improve the system's reliability, the four barriers are axisymmetrically placed in two layers, two barriers for each layer, to constitute a double-layer structure with a thickness of 100 μm. The ignition test results show that the S&A device can prevent the initiator from detonating the lead charge in safety condition. In arming condition, the lead charge will be detonated.  相似文献   
973.
《防务技术》2022,18(9):1538-1545
3-nitro-1,2,4-tri-azol-5-one (NTO) is a high energy insensitive explosive. To study the shock initiation process of NTO-based polymer bonded explosive JEOL-1 (32%octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX), 32% NTO, 28% Al and 8% binder system), the cylinder test, the gap experiments and numerical simulation were carried out. Firstly, we got the detonation velocity (7746 m/s) and the parameters of Jones-Wilkins-Lee (JWL) equation of state (EOS) for detonation product by cylinder test and numerical simulation. Secondly, the Hugoniot curve of unreacted explosive for JEOL-1 was obtained calculating the data of pressure and time at different Lagrangian positions. Then the JWL EOS of unreacted explosive was obtained by utilizing the Hugoniot curve as the reference curve. Finally, we got the pressure growth history of JEOL-1 under shock wave stimulation and the parameters of the ignition and growth reaction rate equation were obtained by the pressure-time curves measured by the shock-initiation gap experiment and numerical simulation. The determined trinomial ignition and growth model (IG model) parameters can be applied to subsequently simulation analysis and design of insensitive ammunition with NTO-based polymer bonded explosive.  相似文献   
974.
《防务技术》2022,18(10):1842-1851
In this study, the approximate and exact solutions for the stationary-state of the solids model with neglecting reactant consumption for both non-uniform and uniform temperature systems were applied on gas ignition under a constant pressure condition. The criticality conditions for a slab, an infinite cylinder, and a sphere are determined and discussed using dimensionless temperatures under constant ambient and surface temperatures for a non-uniform temperature system. Exact solution for a Semenov model with convection heat loss was also presented. The solution of the Semenov problem for constant volume or density as a solid and constant pressure were compared. The critical parameter δ is calculated and compared with those of Frank-Kamenetskii solution values. The validation of the calculated ignition temperatures with other exact solution and experimental results were offered. The relation between critical parameters form Semenov and F.K. models solution was introduced.  相似文献   
975.
The formation mechanism of an EFP(explosively formed projectile) using a double curvature liner under the overpressure effect generated by a regular oblique reflection was investigated in this paper.Based on the detonation wave propagation theory,the change of the incident angle of the detonation wave collision at different positions and the distribution area of the overpressure on the surface of the liner were calculated.Three-dimensional numerical simulations of the formation process of the EFP with tail as well as the ability to penetrate 45# steel were performed using LS-DYNA software,and the EFP ve-locity,the penetration ability,and the forming were assessed via experiments and x-ray photographs.The experimental results coincides with those of the simulations.Results indicate that the collision of the detonation wave was controlled to be a regular oblique reflection acting on the liner by setting the di-mensions of the unit charge and maintaining the pressure at the collision point region at more than 2.4 times the CJ detonation when the incident angle approached the critical angle.The distance from the liner midline to the boundary of the area within which the pressure ratio of the regular oblique reflection pressure to the CJ detonation pressure was greater than 2.5,2,and 1.5was approximately 0.66 mm,1.32 mm,and 3.3 mm,respectively.It is noted that pressure gradient caused the liner to turn inside out in the middle to form the head of the EFP and close the two tails of the EFP at approximately 120μs.The penetration depth of the EFP into a 45# steel target exceeded 30 mm,and there was radial expansion between the head and tail of the EFE increasing the penetration resistance of the EFP.Therefore,the structural size of the unit charge and the liner can be further optimized to reduce resistance to increase the penetration ability of the EFP.  相似文献   
976.
In terrorism research, three different sources of information and data exist: the terrorists and their environment; the incidents; and the population. This article discusses the strengths and weaknesses of research that is concerned with, or relies on, any of the mentioned sources. An in-depth understanding of the methodological issues that come with these sources is important to correctly interpret results from scientific studies. It is highlighted how the different scientific approaches add to a holistic view of terrorism as a phenomenon. Furthermore, the double-edged sword of information in the field of terrorism is discussed. From these deliberations, guidance concerning the future work of both scholars and decision-makers can be deducted.  相似文献   
977.
2012年1月5日,美国国防部发表了《保持美国的全球领导地位:21世纪的防务重点计划报告》,在"重返亚太"战略的战略背景下,重点针对美国未来的军事力量结构、全球部署态势、军事战略目标等进行了重新规划。新军事战略调整对整个国际格局和地区性大国产生深远影响。随着美国重返亚太的战略调整,军事上的相互依赖程度体现在美日同盟之间尤为突出。本文仅从军事战略角度,运用《权力与相互依赖》中部分理论对其调整下的美日军事同盟机制进行分析。  相似文献   
978.
当代科技进步不仅影响着世界格局的变革,也深刻影响着国家的外交行为。随着中国经济实力和科技实力的快速发展,中国更为主动、自信地以大国身份融入国际社会,在几乎所有重要的全球性国际机制中都发挥着积极作用,遵守和履行相应的规则和义务,承担为国际社会提供公共产品以及维护正常合理的国际秩序等国际责任。但随着全球问题的不断增多,国际社会对中国承担更多国际责任的期待也在增多,有些西方国家甚至要求中国承担超出能力的国际责任。面对错综复杂的新形势,中国应该清醒认识自身的国际角色定位,在确保自身崛起的前提下,以科技实力和综合国力承担起力所能及的国际责任,为中国的和平发展提供更广泛的认同基础。  相似文献   
979.
军民融合式发展是实现富国与强军相统一的必由之路,也是增强国防动员潜力、提高国防动员能力的有效途径。在新的形势下推进国防动员建设,必须进一步强化军民融合观念,完善军民融合机制,提高军民融合层次,增强军民融合实效,努力促进动员潜力随经济实力同步增长、动员能力随需求拓展不断提升,实现经济效益、社会效益与国防效益有机统一。  相似文献   
980.
量子保密通信是利用量子力学的基本原理来实现信息无条件安全传递的一种全新密码方法,其核心是量子密钥分发。2014年正好是量子保密通信的第一个协议—BB84协议提出30周年。经过30年的发展,量子保密通信在理论和实验上都得到了快速发展,实际工程应用也初具规模。文章对量子保密通信的历史发展及研究现状进行了简要回顾,特别介绍了基于实际量子保密通信系统的量子黑客和防御。最后,对未来的几个研究方向进行了简要讨论。  相似文献   
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