首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   18649篇
  免费   54篇
  国内免费   125篇
航空   9970篇
航天技术   5653篇
综合类   255篇
航天   2950篇
  2021年   161篇
  2018年   224篇
  2016年   159篇
  2014年   442篇
  2013年   523篇
  2012年   426篇
  2011年   595篇
  2010年   408篇
  2009年   757篇
  2008年   806篇
  2007年   382篇
  2006年   431篇
  2005年   404篇
  2004年   451篇
  2003年   563篇
  2002年   492篇
  2001年   595篇
  2000年   378篇
  1999年   463篇
  1998年   461篇
  1997年   336篇
  1996年   410篇
  1995年   489篇
  1994年   488篇
  1993年   361篇
  1992年   361篇
  1991年   251篇
  1990年   240篇
  1989年   433篇
  1988年   212篇
  1987年   244篇
  1986年   244篇
  1985年   652篇
  1984年   529篇
  1983年   422篇
  1982年   491篇
  1981年   614篇
  1980年   248篇
  1979年   190篇
  1978年   189篇
  1977年   146篇
  1976年   155篇
  1975年   196篇
  1974年   180篇
  1973年   161篇
  1972年   188篇
  1971年   148篇
  1970年   143篇
  1969年   147篇
  1967年   142篇
排序方式: 共有10000条查询结果,搜索用时 0 毫秒
991.
Remote sensing scientists work under assumptions that should not be taken for granted and should, therefore, be challenged. These assumptions include the following:1. Space, especially Low Earth Orbit (LEO), will always be available to governmental and commercial space entities that launch Earth remote sensing missions.2. Space launches are benign with respect to environmental impacts.3. Minimization of Type 1 error, which provides increased confidence in the experimental outcome, is the best way to assess the significance of environmental change.4. Large-area remote sensing investigations, i.e. national, continental, global studies, are best done from space.5. National space missions should trump international, cooperative space missions to ensure national control and distribution of the data products.At best, all of these points are arguable, and in some cases, they're wrong. Development of observational space systems that are compatible with sustainability principles should be a primary concern when Earth remote sensing space systems are envisioned, designed, and launched. The discussion is based on the hypothesis that reducing the environmental impacts of the data acquisition step, which is at the very beginning of the information stream leading to decision and action, will enhance coherence in the information stream and strengthen the capacity of measurement processes to meet their stated functional goal, i.e. sustainable management of Earth resources. We suggest that unconventional points of view should be adopted and when appropriate, remedial measures considered that could help to reduce the environmental footprint of space remote sensing and of Earth observation and monitoring systems in general. This article discusses these five assumptions in the context of sustainable management of Earth's resources. Taking each assumption in turn, we find the following:(1) Space debris may limit access to Low Earth Orbit over the next decades.(2) Relatively speaking, given that they're rare event, space launches may be benign, but study is merited on upper stratospheric and exospheric layers given the chemical activity associated with rocket combustion by-products.(3) Minimization of Type II error should be considered in situations where minimization of Type I error greatly hampers or precludes our ability to correct the environmental condition being studied.(4) In certain situations, airborne collects may be less expensive and more environmentally benign, and comparative studies should be done to determine which path is wisest.(5) International cooperation and data sharing will reduce instrument and launch costs and mission redundancy. Given fiscal concerns of most of the major space agencies – e.g. NASA, ESA, CNES – it seems prudent to combine resources.  相似文献   
992.
Eiges  P. E.  Zastenker  G. N.  Safrankova  J.  Nemecek  Z.  Eismont  N. A. 《Cosmic Research》2001,39(5):432-438
Based on simultaneous measurements of ion fluxes made onboard the closely separated satellites Interball-1and Magion-4, the propagation velocity of middle-scale plasma structures in the Earth's foreshock relative to the solar wind flow is estimated. The derived value of this velocity allows these structures to be identified as a fast magnetosonic wave propagating upstream of the solar wind inflowing the Earth's bow shock. An evaluation is also made of the correlation length of these disturbances in the plane perpendicular to the Sun–Earth line. This length is approximately equal to 2R E.  相似文献   
993.
输油管道泄漏自动检测装置的研制   总被引:3,自引:0,他引:3  
介绍一种基于软件的管道泄漏自动检测装置 ,通过检测压力、流量、温度等的变化来判断泄漏是否发生及发生泄漏的位置。该装置具有适应性广、安装简单等优点。  相似文献   
994.
RDX/AP/HTPB推进剂热分解特性研究   总被引:2,自引:0,他引:2  
利用高压差示扫描量热仪(PDSC)研究了RDX/AP/HTPB推进剂系列配方的热分解性能,发现配方组分的改变对RDX/AP/HTPB推进剂的热分解性能有影响,突出表现在RDX/AP/HTPB推进剂中RDX分解峰变宽,AP放热分解效应增强。推进剂中添加Al粉后,RDX的分解受到抑制,而AP的分解却得到增强。  相似文献   
995.
Zetzer  J. I.  Kozlov  S. I.  Rybakov  V. A.  Ponomarenko  A. V.  Smirnova  N. V.  Romanovsky  Yu. A.  Meng  C.-I.  Erlandson  R.  Stoyanov  B. 《Cosmic Research》2002,40(3):233-240
The measurements of infrared emission from an artificial structure, which was generated during the Fluxus experiment with plasma jet injection into the atmosphere, are obtained and discussed for the first time. Additional experimental data on the airglow in the visible spectral band of the disturbed region of the atmosphere are presented. A generalized analysis of the data is given.  相似文献   
996.
This report is an initial review of plans for a extensive program to survey and develop the Moon and to explore the planet Mars during the 21st century. It presents current typical plans for separate, associated and fully integrated programs of Lunar and Martian research, exploration and development, and concludes that detailed integrated plans must be prepared and be subject to formal criticism. Before responsible politicians approve a new thrust into space they will demand attractive, defensible, and detailed proposals that explain the WHEN, HOW and WHY of each stage of an expanded program of 21st century space research, development and exploration. In particular, the claims of daring, innovative, but untried systems must be compared with the known performance of existing technologies. The time has come to supersede the present haphazard approach to strategic space studies with a formal international structure to plan for future advanced space missions under the aegis of the world's national space agencies, and supported by governments and the corporate sector.  相似文献   
997.
石墨渗铜喉衬的烧蚀特性   总被引:7,自引:0,他引:7  
介绍了石墨渗铜材料作为固体火箭发动机(SRM)喉衬与.长尾管衬套的烧蚀特性和机理。液态铜在高温高压燃气的作用下仍滞留在石墨基材内,起到抑制烧蚀的效果,改善了KS-8高强石墨的耐烧蚀性能。  相似文献   
998.
在丁羟/铝粉/高氯酸铵组成的三组元推进剂体系中,通过药浆流变性测试、动态力学分析(DMA)、单向拉伸性能、凝胶分数和相对交联密度的测定,研究了一些功能组分如氮丙啶类化合物MAPO、醇胺络合物TEA·BF3、胺类化合物H对推进剂工艺性能和力学性能的影响.结果表明,MAPO可以降低药浆屈服值和表观粘度,改善工艺性能,显著增加最大抗拉强度,但对最大伸长率无影响;TEA·BF3大幅度增加药浆屈服值,使工艺性能变差,一定程度上提高最大抗拉强度和发挥熵弹性而增加最大伸长率,H可以显著改善推进剂工艺性能和增加最大伸长率.文中还对功能组分在推进剂中的作用机理进行了分析探讨.  相似文献   
999.
丁羟推进剂粘合剂网络结构调控方法探讨   总被引:4,自引:2,他引:4  
把扩链剂的使用作为调整丁羟推进剂粘合剂网络及其形态结构的一个重要手段。采用扩链剂、交联剂和真实固化参数(Rt)等综合的方法调控丁羟推进剂性能,可望比单纯控制名义固化参数(Ro)获得更好的力学性能及其稳定性。推导了丁羟推进剂粘合剂系统网络调整的通用计算公式和各种特定条件下的计算公式。  相似文献   
1000.
多目标多光谱高温仪的研制   总被引:1,自引:0,他引:1  
根据固体火箭发动机羽焰特征研制了多目标多光谱高温仪。文中介绍了多光谱测温技术及测温仪系统构成。该系统可同时测量羽焰6个目标点的温度,每个目标点均有8个工作波长,可实现对发动机试验时羽焰流场轴向和环向多目标的温度动态测量。  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号