Recent progress on transition metal oxides and carbon-supported transition metal oxides as catalysts for thermal decomposition of ammonium perchlorate

As a main oxidizer in solid composite propellants, ammonium perchlorate (AP) plays an important role because its thermal decomposition behavior has a direct influence on the characteristic of solid com-posite propellants. To improve the performance of solid composite propellant, it is necessary to take measures to modify the thermal decomposition behavior of AP. In recent years, transition metal oxides and carbon-supported transition metal oxides have drawn considerable attention due to their extraor-dinary catalytic activity. In this review, we highlight strategies to enhance the thermal decomposition of AP by tuning morphology, varying the types of metal ion, and coupling with carbon analogue. The enhanced catalytic performance can be ascribed to synergistic effect, increased surface area, more exposed active sites, and accelerated electron transportation and so on. The mechanism of AP decom-position mixed with catalyst has also been briefly summarized. Finally, a conclusive outlook and possible research directions are suggested to address challenges such as lacking practical application in actual formulation of solid composite propellant and batch manufacturing.     

Survivability assessment of spacecraft impacted by orbit debris

To help optimize the spacecraft design and reduce the risk of spacecraft mission failure, a new approach to assess the survivability of spacecraft in orbit is presented here, including the following three steps:1) Sensitivity Analysis of spacecraft. A new sensitivity analysis method, a ray method based on virtual outer wall, is presented here. Using rays to simulate the debris cloud can effectively address the component shadowing issues. 2) Component Vulnerability analysis of spacecraft. A function"Component functional reduction degree — Component physical damage degree"is provided here to clearly describe the component functional reduction. 3) System-level Survivability Assessment of spacecraft. A new method based on expert knowledge reasoning, instead of traditional artificial failure tree method, is presented here to greatly improve the efficiency and accuracy of calculation.     

双转子活塞发动机工作过程的数值模拟

双转子活塞发动机是一种新型的差速式转子发动机,与传统发动机相比较具有很多优点,如不需要复杂的阀门装置,而且功率密度更高等。为了分析和研究双转子活塞发动机的运行特性,针对该发动机工作循环的热力学过程建立了其零维模型,确定了主要的边界条件,运用Matlab/simulink进行了数值模拟。对应不同的主轴转角,计算出气缸内工质的质量值、压力值和温度值。基于算得的压力值,求取了该发动机的平均指示压力和功重比等参数,与传统发动机相比较,双转子活塞发动机气缸工作容积的利用程度更大,整体结构更加紧凑。     

车载光学测量设备任务调度问题建模与求解

为提高观测方案效费比、改进探测能力,探索了一类车载光学测量设备的观测任务调度问题,并给出了解决方案。将观测任务调度问题建模为一个寻找最优观测方案的数学问题,结合设备的性能特点,给出了观测方案的数学描述,梳理了观测方案应满足的约束,提出了评价观测方案质量的指标,进而利用多属性决策方法来计算不同方案的总体效能,并排序获得最优方案。仿真算例验证了方法的有效性,相关研究成果对车载光学测量设备的运用实践具有一定的参考价值。     

单脉冲星自主导航的可行性分析

在全面分析美国X射线脉冲星自主导航(XNAV)计划和国内外相关研究的基础上,提出了我国在现阶段实施"单脉冲星自主导航"计划的建议.认为无论是国防建设和经济建设的战略需求,还是我国现阶段的科学技术研究基础,实施这一计划都是必要与可行的.     

等离子体技术在核化生洗消中的应用研究

等离子体技术是一种高效、快速的污染消除技术,在核化生洗消领域表现出良好的应用前景,国内外都在对其进行广泛而深入的研究。综述了近年来国内外等离子体技术在核化生洗消领域的研究情况,并提出了该技术应用于洗消领域尚需解决的问题和发展趋势。     

隧道火灾快速补救方法研究

通过对多个隧道火灾事故案例及火灾特点的分析,结合我国目前铁路和公路隧道情况,提出了一种利用涡喷消防装备快速扑灭隧道火灾的方法,实践证明该方法扑灭隧道火灾快速有效。     

遗传算法处理导弹一体化优化中隐式约束问题探讨

在详细分析模式定理及典型遗传算法运行机理基础上,针对"隐式约束"问题,创造性地对其进行了适应性改造,并证明了其收敛性。仿真算例及工程实践问题表明,该方法有极强的全局寻优及高速收敛能力,是值得推荐使用的有效方法之一。     

制定会计电算化管理办法的几点建议

在会计电算化普及的今天,制定一套既符合现今会计制度,适应自身情况又行之有效的会计电算化管理办法,是增强高校会计电算化工作的科学性、规范性及效率性的前提条件。     

带可控整流负载的三相同步发电机的解析计算

在广泛应用的交流发电机整流系统中,对其可控时的稳态特性进行了解析计算.考虑了等效电路中电枢电阻对电压关系的影响,得出了实用的解析计算公式,并给出了计算步骤.实验证明,该结果具有较高的精度.