航天创意产业园区发展问题探讨

本文分析了航天创意产业园建设存在的问题,探讨了航天创意产业园区建设的模式和途径。     

京津冀一体化背景下河北产业园区人才聚集与对策研究

在京津冀一体化协同发展的必然趋势下,河北地区在整体科技技术水平、科研创新能力和科技人才吸引存在着明显的差距,因此建立拥有良好的科技人才聚集环境的产业园区,吸纳京津地区科技应用人才,发挥好作为京津冀地区科技产业应用和推广的作用,成为河北省推进京津冀科技协调发展的重要工作。文章从地理环境因素、文化环境因素、制度环境因素、科技环境因素和市场环境因素五个方面对现阶段河北产业园区人才聚集环境现状进行分析,并从宏观和微观两大方面提出提升人才聚集环境的对策。     

浅析航天创意产业品牌文化

本文通过对航天创意产业品牌文化建设的介绍,总结了航天创意产业的特点,提出了航天创意产业品牌建设应该具备的要素,以及进行航天创意产业品牌建设应采取的基本策略。     

河北省卫星导航产业发展的SWOT分析

近几年,很多国家和地区都在大力发展卫星导航产业,河北省自十一五以来,也坚持把卫星导航产业作为省内重点发展和培育的产业之一。本文通过对河北省发展卫星导航产业进行了SWOT分析的基础上,提出了加快河北省卫星导航产业发展的战略举措。     

创意产业人才发展的现状及对策研究

经济的发展促进了经济结构的升级,创意产业也伴随着消费者需求结构的改变和技术水平的发展而快速发展起来,创意产业的发展一方面需要需求的拉动,但另一方面也需要具备足够的供给条件才能够取得理想效果,在创意产业的发展中,创意人才的地位至关重要,只有培养大量高素质的创意人才,才能够保证创意产业长期健康的发展。     

河北省发展航天产业后发争先的路径分析

本文分析了河北省发展航天产业的后发优势,探索了河北省发展航天产业后发争先的路径。     

开拓航天文化创意产业 迎接太空经济新时代

<正>文化创意产业起源于后工业化的发达国家,前景广阔,被公认为21世纪全球经济一体化时代的朝阳产业和黄金产业。英国创意产业之父约翰·霍金斯在《创意经济》一书中指出:纵观全球,发达国家的众多创意产品、营销、服务,吸引了全世界     

河北省高新技术产业集群绩效评价研究

本文首先介绍了河北省高新技术产业集群的发展现状,指出绩效评价的重要性。根据确定的绩效评价原则,采用层次分析法(AHP)和模糊综合评价法结合相关统计、调研数据对河北省高新技术产业集群进行绩效评价,得出河北省高新技术产业集群绩效属于中等水平的结论,存在着不足,并提出了促进河北省高新技术产业聚集发展的对策。     

河北旅游资源深度挖掘:与文化、科技融合发展

旅游业只有与文化、科技融合发展,才能真正做大做强。本文借鉴兄弟省市推动旅游与文化、科技融合发展的成功经验,分析河北省旅游与文化、科技融合发展的现状,提出了推动河北省旅游与文化、科技融合发展的具体举措。     

河北承接高新高端产业转移对接路径研究

京津冀协同发展上升到国家战略以来,河北各地在承接京津转移产业时不是所有产业都要承接,那些不利于自身持续发展的低端产业和落后产能,也会有选择的承接,而且在承接北京转移产业时还要面对天津的竞争,不是想承接就能承接上,这就需要一个科学的、系统的考量。基于此,本论文结合河北省实际,明确河北省可以承接哪些高新高端产业,并确定河北及各地市承接转移高新高端产业的具体类别;最后,借助系统论思维,综合上述已有研究结论,以及河北省及各地实际,从硬环境建设、软环境建设和竞争性环境建设方面,提出具体的承接政策建议,从而为相关政策措施等的健全完善,提供借鉴和参考。     

GEOS and its US and European components: Challenges and impact

The Centre Français sur les Etats Unis (CFE) held a day-long workshop on GEOSS, GMES and IEOS on 17 January 2006. Sponsored by Arianespace, the invitation-only roundtable drew some 50 participants from European and US administration, industry and academia. The programme and the presentations are on the CFE web site: www.cfe-ifri.net. This report summarizes the proceedings.     

偶氮呋咱和氧化偶氮呋咱的合成及表征

介绍了高能材料二氨基偶氮呋咱(DAAF)、二氨基氧化偶氮呋咱(DAOAF)及二硝基氧化偶氮呋咱(DNOAF)的合成。其中,采用新型氧化剂制备DAAF,得率提高至65.60%。通过DSC-TG、元素分析、IR、1H NMR和MS等方法,对其结构进行了鉴定,并进行了常规的感度测试。感度数据表明,无氢炸药DNOAF的摩擦感度较大,与C-12相当,而DAAF和DAOAF为低感度炸药。     

教育教学活动中的师生人际冲突及其解决方法

受传统观念的影响,人们一般只看到师生人际冲突的负面影响,而很少注意其正面作用;实际上,师生人际冲突是教育教学的互动形式之一,它的存在是必然的,也是合理的,它既有消极有害的一面,也有积极有益的一面。文章试在分析师生人际冲突原因的基础上,针对其影响的二重性,从学校、教师、学生三个方面,提出了正确对待师生人际冲突的建设性对策。     

汽车检测与维护专业建设的回顾与总结

汽车检测与维护专业是我校重点建设的广西区区级示范专业,经过五年的建设已经形成了一定的规模。文章主要从实验实训中心建设、课程建设、教材建设、师资队伍建设、教学改革等方面对该专业的建设历程进行了回顾和总结。     

Atlas II and IIA analyses and environments validation

General Dynamics has now flown all four versions of the Atlas commercial launch vehicle, which cover a payload weight capability to geosynchronous transfer orbit (GTO) in the range of 5000–8000 lb. The key analyses to set design and environmental test parameters for the vehicle modifications and the ground and flight test data that validated them were prepared in paper IAF-91-170 for the first version, Atlas I.

This paper presents similar data for the next two versions, Atlas II and IIA. The Atlas II has propellant tanks lengthened by 12 ft and is boosted by MA-5A rocket engines uprated to 474,000 lb liftoff thrust. GTO payload capability is 6225 lb with the 11-ft fairing. The Atlas IIA is an Atlas II with uprated RL10A-4 engines on the lengthened Centaur II upper stage. The two 20,800 lb thrust, 449 s specific impulse engines with an optional extendible nozzle increase payload capability to GTO to 6635 lb. The paper describes design parameters and validated test results for many other improvements that have generally provided greater capability at less cost, weight and complexity and better reliability. Those described include: moving the MA-5A start system to the ground, replacing the vernier engines with a simple 50 lb thrust on-off hydrazine roll control system, addition of a POGO suppressor, replacement of Centaur jettisonable insulation panels with fixed foam, a new inertial navigation unit (INU) that combines in one package a ring-laser gyro based strapdown guidance system with two MIL-STD-1750A processors, redundant MIL-STD-1553 data bus interfaces, robust Ada-based software and a new Al-Li payload adapter. Payload environment is shown to be essentially unchanged from previous Atlas vehicles. Validation of load, stability, control and pressurization requirements for the larger vehicle is discussed.

All flights to date (five Atlas II, one Atlas IIA) have been successful in launching satellites for EUTELSAT, the U.S. Air Force and INTELSAT. Significant design parameters validated by these flights are presented. Particularly noteworthy has been the performance of the INU, which has provided average GTO insertion errors of only 10 miles apogee, 0.2 miles perigee and 0.004 degrees inclination. It is concluded that Atlas II/IIA have successfully demonstrated probably the largest number of current state-of-the-art components of any expendable launch vehicle flying today.     

Launch and early operations of Herschel and Planck

On 14 May 2009 the European Space Agency launched 2 space observatories: Herschel (with a 3.5 m mirror it is the largest space telescope ever) will collect long-wavelength infrared radiation and will be the only space observatory to cover the spectral range from far-infrared to sub-millimetre wavelengths, and Planck will look back at the dawn of time, close to the Big Bang, and will examine the Cosmic Microwave Background (CMB) radiation to a sensitivity, angular resolution and frequency range never achieved before. This paper will present the Flight Dynamics, mission analysis challenges and flight results from the first 3 months of these missions.Both satellites were launched on the same Ariane 5 and travelled to the L2 Lagrange point of the sun–earth system 1.5 million km from the earth in the opposite direction of the sun. There they were injected to a quasi-halo orbit (Herschel) with the dimension of typically 750,000 km×450,000 km, and a Lissajous orbit (Planck) of 300,000 km×300,000 km.In order to reach these Lissajous orbits it is mandatory to perform large trajectory correction manoeuvres during the first days of the mission. Herschel had its main manoeuvres on the first day. Planck had to be navigated on the first day and by a mid-course correction manoeuvre, the L2 orbit insertion manoeuvre was planned on day 50. If these slots were missed, fuel penalties would rapidly increase.This posed a heavy load on the operations teams because both spacecrafts have to be thoroughly checked out and put into the correct modes of their attitude control systems during the first hours after launch.The sequence of events will be presented and explained and the orbit determination results as well as the manoeuvre planning will be emphasised.     

月球测绘学分类及应用展望

根据月球测绘的研究现状及发展趋势,对月球测绘学的概念进行了溯源与拓展。在分析月球测绘学与地球测绘学主要差异基础上,从传统测绘学科分类角度出发,综合考虑月球测绘学特殊性,重新梳理出月球测绘学主要学科专业分类,并详细介绍了每个学科专业的定义及国内外研究现状,给出了月球测绘学的五个主要应用领域及其应用展望。我国应尽早开展月球测绘理论与技术研究,形成完整的月球测绘学科体系,能够有力地促进我国空间科学技术的发展,保障后续探月工程的顺利实施。     

英汉词语空缺与跨文化差异及翻译策略探究

语言是文化的载体,文化上的差异导致了英汉语言中的词汇空缺现象,词汇空缺现象反映了语言的民族性。在跨文化交际中,词汇空缺会给交际带来障碍,造成语用失误,甚至导致交际失败,论文就词语的空缺现象与跨文化差异中的翻译策略进行了一些探讨。     

SMOS与Aquarius卫星海表盐度测量方法及数据的对比分析

国际上发射的海表盐度遥感卫星主要有2颗:欧洲的SMOS和美国的Aquarius卫星,为给后续海表盐度遥感提供参考借鉴,对比分析了这2颗卫星的遥感器载荷、数据处理算法和盐度数据。遥感器载荷方面,SMOS采用L波段二维综合孔径辐射计,而Aquarius采用L波段实孔径辐射计加散射计;数据处理算法方面,分析了二者在介电常数模型、海面粗糙度校正以及反演算法方面的差异;盐度数据方面,分析了SMOS与Aquarius盐度数据之间的相关程度,并分别与ISAS(In Situ Analysis System)浮标盐度数据作对比,分析了2颗卫星的盐度数据精度。将2颗卫星的盐度遥感数据与ISAS浮标盐度数据对比发现,在全球范围内,Aquarius盐度测量精度优于SMOS;但在开阔海域,SMOS盐度测量精度优于Aquarius;而在近海岸区域,均出现较大的误差,且SMOS数据误差更大。     

凝胶推进剂及其模拟剂的制备和特性表征

高能凝胶推进剂的选择、制备、实验及特性表征是凝胶推进剂研究的关键环节.燃料凝胶化包括有机和无机两种胶凝剂.氧化剂的凝胶化使用了无机胶凝剂.此外选择和配制了凝胶推进剂的模拟剂,它具有与实际燃料和氧化剂相匹配的流变特性.制备了在流变学上相匹配的凝胶燃料和凝胶氧化剂、惰性凝胶模拟剂与凝胶推进剂,并对其流变学特性进行了分类.