基于湿热老化试验的NEPE推进剂贮存寿命预估

用NEPE推进剂进行湿热加速老化试验获得了推进剂在不同湿热老化条件下抗拉强度和弹性模量随老化时间的变化规律,建立了推进剂湿热老化失效物理模型,并提出了将弹性模量作为失效判据预估推进剂贮存寿命的方法。分别用抗拉强度和弹性模量作为失效判据,对推进剂贮存寿命进行估算。结果表明：将弹性模量作为失效判据预估NEPE推进剂贮存寿命的方法可行。     

卫星太阳电池翼分子污染量模拟计算研究

文章介绍了太阳电池翼分子污染预估模拟的研究方案,包括分子污染源动力模拟、分子污染沉积过程模拟和分子污染传输过程模拟。根据所建立的污染模型,对“东方红”系列某卫星的太阳电池翼进行分析,得到分子分布密度和能量等值线图。     

航天用电连接器的接触可靠性研究

接触可靠性是保证航天用电连接器正常工作的关键。结合近年来在检验及使用过程中出现的多想航天用电连接器接触失效的实例，在阐明其失效机理基础上，分析了影响电连接器接触可靠性的各种因素，并对分离力等接触可靠性检查方法进行了讨论。     

空间旋转目标涡流消旋概念与仿真分析

针对消除空间旋转目标姿态旋转的问题,本文将第二代高温超导技术与涡流制动技术相结合,提出超导式涡流消旋的概念。然后,对涡流消旋的技术可行性进行了定性分析,通过对多种消旋技术手段的权衡比较归纳出涡流消旋的优势。接着,采用电磁张量理论,建立了电磁-涡流作用机理的精确磁场和涡流力矩模型;最后,考虑实际消旋的任务需求,对典型的高速旋转目标、低速旋转目标、以及复合旋转目标的消旋进行了动力学仿真研究。仿真结果表明,涡流消旋具有足够强大的制动能力,能有效消除目标的高速旋转或复合旋转运动。     

电缆支承拖链传动运动分析

电缆支承拖链是一种特种链条,用以支承生产机械中的电缆,油,气,水等挠性管理,实现可动的导向。运动特性是设计电缆支承拖链传动的重要理论基础。本文籍机械运动简图建立了运动方程,并对正确选用主要设计参数以降低传动的不均匀系数作了定量的分析研究,结果表明其效果非常显著。     

小子样下导电滑环磨损失效仿真的可靠性评估研究

针对滑环失效数据较少的特点，构建导电滑环磨损失效模型，结合小子样数据处理法和随机性理论对滑环摩擦副进行可靠性评估研究。首先，考虑滑环摩擦副在热力电多场耦合环境下的特点，应用传热学、赫兹理论、能量守恒定律量化多场耦合对滑环摩擦副的影响，再结合Archard模型理论构建导电滑环摩擦副磨损失效模型。然后，采用小子样数据的虚拟增广法和Boot-strap法对仿真数据进行扩展，根据滑环磨损特征量分布规律分别得到随机失效阈值与固定阈值下的可靠度函数曲线，以某厂制造的导电滑环为例，进行滑环摩擦副可靠性评估，实验结果表明随机失效阈值下的可靠度与实际更接近。研究表明所构建的磨损模型和方法可以有效地对导电滑环进行可靠性评估，避免了传统的必须依赖大量试验数据的方法，解决了缺少滑环试验数据而难以进行可靠性评估的问题，填补了导电滑环可靠性研究的空白。     

复合材料连接方法

文中叙述了复合材料常用的几种连接方法,分析了各种连接的破坏模式和连接形式的选择,同时还介绍了国外复合材料连接方法新进展等内容。     

Multi-objective optimization of different dome reinforcement methods for composite cases

A multi-objective optimization method was proposed for different dome reinforcement methods of a filament-wound solid rocket motor composite case based on a Radial Basis Function (RBF) model. Progressive damage of the composite case was considered in a simulation based on Hashin failure criteria, and simulation results were validated by hydraulic burst tests to precisely predict the failure mode, failure position, and burst pressure. An RBF surrogate model was established and evaluated by Relative Average Absolute Error (RAAE), Relative Maximum Absolute Error (RMAE), Root Mean Squared Error (RMSE), and R² methods to improve the optimization efficient of dome reinforcement. In addition, the Non-dominated Sorting Genetic Algorithm (NSGA-II) was employed to establish multi-objective optimization models of variable-angle and variable-polar-radius dome reinforcements to investigate the coupling effect of the reinforcement angle, reinforcement layers, and reinforcement range on the case performance. Optimal reinforcement parameters were obtained and used to establish a progressive damage model of the composite case with dome reinforcement. In accordance with progressive damage analysis, the burst pressure and performance factor were obtained. Results illustrated that variable-angle dome reinforcement was the optimal reinforcement method compared with variable-polar-radius dome reinforcement as it could not only ensure the reinforcement angle’s continuous changing but also decrease the mass of composite materials. Compared with the unreinforced case, the reinforced case exhibited an increase in the burst pressure and performance factor of 36.1% and 23.5%, respectively.     

可靠性增长试验的计划曲线及其参数研究

在用杜安（Ｄｕａｎｅ）增长模型制定可靠性增长试验的计划曲线时，确定总试验时间经常会遇到缺乏数据、经验和经费不足等困难。本文利用杜安增长模型导出了总试验时间的计算公式，并对影响总试验时间的诸参数进行了分析，提出了选取这些参数的原则和方法，对制定具体的计划曲线有一定的指导意义。     

An archival study of extended X-ray emission from classical and recurrent novae

I discuss morphology and spectrum of the first resolved and detected classical nova shell in the X-rays – the remnant of GK Persei (1901). The existence of such a nebulosity brings about the possibility of other nova remnants emitting X-rays. I calculate that the X-ray luminosity should be about 10²⁶–10³³ ergs s⁻¹ on the onset of cooling for nova remnants. I have done an archival search on 250 classical and recurrent nova candidates using Chandra, XMM-Newton, ROSAT and ASCA databases. There is no significant extended emission detected which places an upper limit of F_x < × 10⁻¹² erg s⁻¹ cm⁻² (unabsorbed). Only exceptions are GK Per, RR Pic and DQ Her (all observed by Chandra ACIS-S and GK Per also by ROSAT HRI) where the latter two show marginal extended emission in the X-rays associated with emission knots (DQ Her) or an equatorial ring (RR Pic).