Research on a MEMS pyrotechnic with a double-layer barrier safety and arming device

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.     

Shock initiation performance of NTO-based polymer bonded explosive

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.     

Thermal explosion of a reactive gas mixture at constant pressure for non-uniform and uniform temperature systems

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.     

非对称相互依赖下的美日军事同盟机制分析——以奥巴马政府“重返亚太”为视角

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。     

试论科技进步与中国国际责任的现实担当

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。     

推进国防动员军民融合深度发展的对策思考

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。     

量子保密通信技术前沿述评

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。     

舰船随舰备件配置方法

为准确预测备件需求数量,需要针对具体的保障对象和保障环境特点,选择合适的评价保障指标。针对单舰船在海上执行训练任务时的随舰备件保障问题,在分析影响随舰备件配置各因素的基础上,通过比较分析各评价保障指标的适用特点,选择满足率作为随舰备件的评价保障指标,进而给出了基于满足率模型的单备件配置方法,为部队装备保障人员合理制定备件保障方案提供决策依据。     

PID调节下H桥式逆变器离散建模及分岔现象

为研究PID调节下H桥式逆变器的非线性行为,选取逆变器输入电压为分岔参数,利用频闪映射法推导出PID调节下H桥式逆变器的离散数学模型.使用Matlab编程得到系统输出电流随输入电压变化的动态分岔图,通过数值仿真验证了离散数学模型的正确性.仿真结果表明频闪映射法适用于建立H桥式逆变器的离散数学模型;PID调节下H桥式逆变器存在分岔行为.研究结果可为建立PID调节下H桥式逆变器的离散数学模型提供参考.     

未来数字化战场中的指挥控制语言研究

针对未来数字化战场中机器人部队指挥控制与协同作战这一新兴研究领域需解决的机-机协同和人-机智能融合等问题,综述国内外相关领域的研究现状,分析了构建我军指挥控制语言的必要性,研究了机器人部队指挥控制语言的技术架构与关键技术,并提出了指挥控制语言的一种形式化语法和语义标注方法和通信协议,并结合海军舰艇作战示例分析了指挥控制语言的可行性及有效性。