走出中国航天民用产业发展的桎梏

正中国航天一贯坚持自力更生,立足自主创新。航天人奋发图强、勇于攀登,与祖国发展同行,创造了中华民族发展史上一个又一个辉煌,为我国军队现代化建设、科技发展、社会经济发展、人才建设、文化建设做出了重大贡献,显著增强了我国国防实力、科技实力、经济实力和民族凝聚力,为实现中华民族伟大复兴谱写了无数航天人的壮丽史诗。航天科学技术的广泛应用,效果显著,带动了我国社会经济的发展,为国民经济建设作出了卓越贡献。     

增强大学生班级凝聚力的几点思考

班级是学生教育管理的重要工具,班级凝聚力建设是培养大学生团队协作意识,提升综合素养的重要途径。作者针对当前高校存在的大学生班级凝聚力缺失问题,分析问题产生的主客观原因,提出了几点思考,旨在提高学生培养质量,促进学生全面发展。     

构建和谐空管企业文化

胡锦涛指出:"当今时代,文化越来越成为民族凝聚力和创造力的重要源泉、越来越成为综合国力竞争的重要因素,丰富精神文化生活越来越成为我国人民的热切愿望。要坚持社会主义先进文化前进     

心有所想

作为一名教育工作者,我有幸参加了"2008年第四届中国航天员体验营延安营"活动。短短的四天时间,令人感受颇深,终生难忘。一直以来,党和国家就把发展航天事业作为推动我国科技事业发展,增强我国经济实力、科技实力、国防实力和民族凝聚力的一项强国兴邦的重大战略举措。从"两弹一星"的震惊世界到"神舟"系列飞船的气冲霄汉,再到"嫦娥"一号的轻舒广袖,揽月问天,一次次雄辩地向世界证明:中国人,了不起!中华民族,是一个正在实现伟大复兴的优秀民族!     

航天发展“十一五”规划

序言 航天是当今世界最具挑战性和广泛带动性的高科技领域之一,航天产业已成为国家的战略高技术产业。发展航天是增强我国经济实力、科技实力、国防实力和民族凝聚力的重要举措。     

我们与神舟遨游太空

2006年10月12日上午9时整,我国神舟六号载人飞船带着华夏儿女期骥的目光腾空而起,冲向太空.神舟六号的成功飞行,标志着我国载人航天工程技术逐步走向成熟,必将极大地增强民族凝聚力,成为激励全国各族人民实现全面建设小康社会奋斗目标的强大动力.作为神舟六号载人飞船各系统配套研制单位,贵州航天电器股份有限公司全体干部员工为神舟六号载人飞船的成功做出了应有的贡献.航天电器人是幸运的,因为实现中华民族千年飞天梦想的伟大创举有我们的参与;航天电器人也是幸福的,因为我们与祖国一起享受到了神六腾空的成功喜悦.     

高校大学生创业团队凝聚力影响因素

近些年来,国家大力提倡“大众创业、万众创新”号召。全国地方高校依托校园的区位优势和资源优势,大多成立校园创业孵化基地,为大学生创业提供便利条件,要想提升在校大学生创业团队创造力和竞争力必须先提高在校大学生创业团队的凝聚力。本文旨在通过对创业的大学生进行问卷调查,分析影响大学生创业团队凝聚力的主观因素和客观因素。并据此提供提升大学生创业团队凝聚力的几点策略。     

如何做好新形势下民航新闻宣传工作

新闻宣传工作是我们党的政治优势,是党的思想政治工作的重要组成部分,是文化建设的有力抓手和重要载体。胡锦涛总书记强调指出,做好新闻宣传工作,关系党和国家工作全局,关系改革和经济社会发展大局,关系国家长治久安。做好民航的新闻宣传工作,是树立行业形象、鼓舞员工士气、增强单位凝聚力、确保安全生产的有力手段。当前,我国经济社会发     

以总体设计部思想助推国家治理体系迈向新高度

正中华民族从站起来、富起来到强起来的伟大飞跃中,始终贯穿着伟大的爱国奋斗精神。近年来,习近平总书记对弘扬爱国奋斗精神作出一系列重要指示,指出"爱国主义是中华民族精神的核心""突破关键核心技术,关键在于有效发挥人的积极性。要发扬光大两弹一星精神,形成良好精神面貌"等。为了深入学习贯彻近平总书记关于弘扬爱国奉献精神的一系列重要指示精神,近日,中央组织部、中央宣传部印发通知,对在广大知识分子中深入开展"弘扬爱国奋斗精神、建功立业新时代"活动作出重要部署。     

坚持质量第一建设中国航天质量文化

从物质层，制度层和精神层等三种表现形态及其之间的联系，制约和渗透的关系，概述了航天质量文化的内涵，分析了建设质量文化是增强航天事业的凝聚力，利用形成约束机制和树立航天产品良好社会形象的重要意义，同时研究和探讨了建设航天质量文化的几种途径。     

On the stability of the track of the space elevator

A string moving with geostationary angular velocity in its radial relative equilibrium configuration around the Earth, reaching from the surface of the Earth far beyond the geostationary height, could be used as track for an Earth to space elevator. This is an old dream of mankind, originating about 100 years ago in Russia. Besides the question of feasibility from a technological point of view also the question concerning the stability of such a configuration has not yet been completely solved. Under the assumption that a proper material (carbon nanotubes) is available, making the connection possible technologically, we address the question of existence and stability of the radial relative equilibrium of a tapered string on a circular geosynchronous trajectory around the Earth, reaching from the surface of the Earth far beyond the geostationary height.     

On the Possibility of the Existence of Volatile Compounds in the Region of the Scott Crater on the Moon

In this paper, we analyze the illumination conditions, the thermal regime, and the possibility of deposits of volatile compounds existing in the vicinity region (NSR S5 region) near the southern pole of the Moon. It has been found that there are no permanently shadowed zones near the Scott crater and the NSR S5 region, though the temperature conditions allow the of compounds such as CH₃OH, SO₂, NH₃, CO₂, H₂S, C₂H₄, and water to remain stable relative to evaporation for a long time (≥1 Gyr). It has been also shown that compounds like CO and CH₄ cannot stably exist in these regions.     

Estimation of the current density and analysis of the geometry of the current system surrounding the Earth

The results of an investigation of the distribution of plasma pressure, pressure gradients, and magnetic field near the equatorial plane in the plasma ring surrounding the Earth under magneto-quiet conditions are presented. Observational data obtained during the international THEMIS mission are used. The picture of the distribution of transverse-current density near the equatorial plane was obtained under assumption of observing the magnetostatic balance condition at geocentric distances from 6 to 12R _E. In estimating the integral transverse current it was accepted that in daytime sector the magnetic-field minima on magnetic field lines are not localized in the equatorial plane. Estimates of the integral transverse current were obtained, which demonstrate the possibility of closing nighttime transverse currents at geocentric distances of up to ～12R _E inside the magnetosphere, which form a high-latitudinal continuation of the ring current.     

对老年人体育锻炼负荷量监控方法的探讨

通过对老年人体育锻炼活动的情况进行相关调查，发现目前老年人体育锻炼中存在一些误区。因此本文针对这些现实情况提出，应根据实际情况运用一些简单易行的方法来对老年人体育锻炼实施医务监督，达到提高老年人体育锻炼的科学性。     

Estimating the accuracy of the technique of reconstructing the rotational motion of a satellite based on the measurements of its angular velocity and the magnetic field of the Earth

The paper has studied the accuracy of the technique that allows the rotational motion of the Earth artificial satellites (AES) to be reconstructed based on the data of onboard measurements of angular velocity vectors and the strength of the Earth magnetic field (EMF). The technique is based on kinematic equations of the rotational motion of a rigid body. Both types of measurement data collected over some time interval have been processed jointly. The angular velocity measurements have been approximated using convenient formulas, which are substituted into the kinematic differential equations for the quaternion that specifies the transition from the body-fixed coordinate system of a satellite to the inertial coordinate system. Thus obtained equations represent a kinematic model of the rotational motion of a satellite. The solution of these equations, which approximate real motion, has been found by the least-square method from the condition of best fitting between the data of measurements of the EMF strength vector and its calculated values. The accuracy of the technique has been estimated by processing the data obtained from the board of the service module of the International Space Station (ISS). The reconstruction of station motion using the aforementioned technique has been compared with the telemetry data on the actual motion of the station. The technique has allowed us to reconstruct the station motion in the orbital orientation mode with a maximum error less than 0.6° and the turns with a maximal error of less than 1.2°.     

实施“三位一体”教育模式 提高学生的综合素质

本文介绍了“三位一体”教育模式的内容,描述亍我们实施该模式所采取的措施及取得的成效。实践表明,“三位一体”教育模式能够提高学生的综合素质,为学生毕业后的发展打下坚实基础,对教育模式的改革具有一定的指导意义。     

从应变计现状看电阻式传感器的前景

电阻式传感器的核心部件——电阻应变计是目前最常用的应力分析的敏感元件。也常用于测量力、压力、扭矩和加速度等物理量。作者简要回顾了电阻应变计的发展历史，介绍了电阻应变计的结构、分类及现状，展望了电阻式传感器的前景。     

System of works on numerical modeling of the dynamics of the structure of the Space Radiotelescope in the RadioAstron project

The results of modeling the dynamics of the Space Radiotelescope are presented. The results of ground-based vibration-dynamic tests are used to validate the calculation models and estimate the damping levels. The dynamic distortions of the reflecting surface caused by the operation of the pointing mechanism of the high-gain antenna are estimated.     

Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits

The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterized by a relatively small perihelion radius and relatively high inclination, which allows one to investigate the polar regions of the Sun. The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.     

复杂受载条件下固体火箭发动机壳体屈曲应力的估计

论文简略介绍了静力轴压下园柱壳屈曲应力的工程计算方法,对某固体火箭发动机壳体的复杂受载条件对壳体屈曲应力的影响进行了分析,并对该火箭发动机壳体屈曲应力如何估计提出了建议。