降低硝胺推进剂燃速和压强指数的暗区增强理论

在分析总结高能硝胺推进剂燃速特性和燃烧火焰结构的基础上，提出了重点降低高压燃速及其压强指数的暗区增强理论；并选择了数种添加剂对上述理论进行了验证。实验结果表明，所选择或合成的添加剂都可同时降低燃速和压强指数；燃烧火焰结构验证实验也表明，加入ＰＣ３０／ＰＣ３５组合添加剂显著增加了暗区的厚度，降低了暗区的压强敏感性和总化学反应级数；同时组合添加剂的抑制作用效率随着压强的增加而增强，这导致推进剂在燃速降     

自硬树脂砂型的开裂原因及防止措施

简述了冷硬树脂砂型在某些情况下的产生开裂的原因及机理，讨论了几种解决的方法，有利于改进产品质量，减少双方的经济损失。     

一种新型空间微小碎片超高速碰撞试验地面模拟方法

文章简要叙述了空间微小碎片环境及其对航天器的影响,同时介绍了一种新型空间微小碎片超高速碰撞地面模拟方法——激光驱动飞片技术。     

Structure and kinetic properties of slow-mode shocks associated with magnetic reconnection in the near-Earth magnetotail

We study the structure and kinetic properties of slow-mode shocks near the plasma sheet boundary layer (PSBL) associated with magnetic reconnection by Cluster observation. The presence of slow-mode shocks is confirmed by traditional Rankine–Hugoniot (RH) analysis and Monte-Carlo shock fitting method. The Walén analysis, applied to the tailward flow associated with slow-mode shocks, also supports that plasma was accelerated across a Petschek-type slow-mode shock connected to the diffusion region. Back-streaming ions were observed on the shock layer, and cold ions were accelerated and heated by slow-mode shocks. In addition, whistler and electrostatic solitary waves were observed around the slow-mode shocks. These waves might be excited by the observed field-aligned electron beams near the shocks.     

J2级经纬仪竖盘指标自动补偿误差不确定度

介绍了按照ＪＪＧ４１４—９４《光学经纬仪》检定、校准Ｊ２级经纬仪竖盘指标自动补偿误差时，依据“’９３国际指南”要求，对其测量不确定度进行的分析、计算。     

Optimum parameter matching obtained by experiments for coring drilling into lunar simulant

This paper performs a series of ground experiments (on the Earth) to obtain optimum parameter matching for a future core drill on the Moon. Three common stages, I, II, III, are recognized with respect to the cut per revolution (CPR), which is defined as the ratio between the feeding speed and the rotating speed. The optimum matching between the feeding speed and the rotating speed for drills locates at the boundary position between Stage II and Stage III, where the coring rate saturates and the weight on the bit and the driving torque are still low. Further data analysis of the ground experiments reveals that the optimum matching signifies a proportional relation between the maximum conveying rate (MCR) by the groove of the auger and its rotating speed. The kinetic analysis in an ideal condition without gravity, the friction from the auger groove and the pressure at the bit confirm a similar proportion. The correlation between the proportions needs further study to determine whether the optimum matching obtained on the ground can be directly applied to future drills on the Moon.     

亚跨超CFD软件平台研制

亚跨ＣＦＤ软件平台研制的宗旨是综合国内外计算流体动力学的最新研究成果，用计算机软件技术的新发展，建立一个面向对象的计算流体动力学的研究开发环境，加快计算流体动力学最新成果向工程应用的转换速度。本文介绍初级版本的研究进展和研究成果，主要匝数值网格生成技术，流场解算器，面向对象的界面设计等三部分组成。     

The Voyager mission Photopolarimeter Experiment

The Voyager Photopolarimeter Experiment is designed to determine the physical properties of particulate matter in the atmospheres of Jupiter, Saturn, and the Rings of Saturn by measuring the intensity and linear polarization of scattered sunlight at eight wavelengths in the 2350–7500 Å region of the spectrum. The experiment will also provide information on the texture and probable composition of the surfaces of the satellites of Jupiter and Saturn and the properties of the sodium cloud around Io. During the planetary encounters a search for optical evidence of electrical discharges (lightning) and auroral activity will also be conducted.     

基于集成学习模型的飞行学员认知负荷研究

在飞行过程中,飞行员需要在短时间内接收大量信息,并做出正确的判断与决策,而过高的认知负荷会影响其感知、判断、决策等认知过程,进而影响飞行安全。首先通过飞行模拟实验获取飞行学员在执行不同飞行任务时的生理数据;然后通过时域、频域分析等方法提取呼吸和心电信号的特征,并通过统计学方法筛选出能够反映认知负荷水平的指标;最后结合支持向量机、K 最邻近、人工神经网络等方法建立集成学习模型,对飞行学员的认知负荷进行评估,并与单一算法进行对比。结果表明：本文建立的集成学习模型具有较高的准确率,能够更好地反映飞行学员认知负荷水平。     

复合固体推进剂过渡相(中间相)力学模型

在总结归纳复合固体推进剂力学性能研究的基础上,吸取键合剂作用模型的优点,结合新近提出的网络与形态结构理论,并引入颗粒充填复合材料中的成熟理论,提出了一个描述复合固体推进剂力学性能的过渡相（中间相）模型。通过力学,数学推导建立了复合固体推进剂的结构因素与力学性能表征参数（σ,ε）的定性关系,这与验证主前人的结果基本一致,其中提出的关于过渡相模量与基体模量匹配的调节方法,为进一步提高复合固体推进剂的力