全文获取类型
收费全文 | 1669篇 |
免费 | 214篇 |
国内免费 | 87篇 |
专业分类
航空 | 301篇 |
航天技术 | 855篇 |
综合类 | 27篇 |
航天 | 787篇 |
出版年
2024年 | 1篇 |
2023年 | 34篇 |
2022年 | 37篇 |
2021年 | 61篇 |
2020年 | 60篇 |
2019年 | 42篇 |
2018年 | 61篇 |
2017年 | 17篇 |
2016年 | 34篇 |
2015年 | 47篇 |
2014年 | 168篇 |
2013年 | 104篇 |
2012年 | 70篇 |
2011年 | 164篇 |
2010年 | 111篇 |
2009年 | 110篇 |
2008年 | 102篇 |
2007年 | 75篇 |
2006年 | 75篇 |
2005年 | 97篇 |
2004年 | 59篇 |
2003年 | 34篇 |
2002年 | 51篇 |
2001年 | 41篇 |
2000年 | 50篇 |
1999年 | 56篇 |
1998年 | 32篇 |
1997年 | 22篇 |
1996年 | 24篇 |
1995年 | 22篇 |
1994年 | 7篇 |
1993年 | 15篇 |
1992年 | 9篇 |
1991年 | 15篇 |
1990年 | 12篇 |
1989年 | 11篇 |
1988年 | 23篇 |
1987年 | 8篇 |
1986年 | 4篇 |
1985年 | 3篇 |
1984年 | 2篇 |
排序方式: 共有1970条查询结果,搜索用时 747 毫秒
501.
J.K. Shi M.N.S. Qureshi S.Z. Ma L.D. Xia J.S. Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2007,40(12):1842-1851
Considering the KuaFu mission, state of the energy release of substorm and storm is simply presented and it’s improvements by KuaFu mission are investigated. The KuaFu mission will provide us an opportunity to improve our understanding of the energy release during the storm and the substorms. The two KuaFu-B satellites flying in 180° phase-lagged formation in a polar orbit will allow synoptic observations of the auroral oval, central plasma sheet, ring current and other regions. It can monitor the polar region 24/7 continuously. The advantage of the KuaFu mission is to provide the data during all phases of storm and substorm time that can be used to study the global energy release during all phases continuously. The data from auroral imager and other in-situ instruments on board KuaFu-B can be used to study the auroral dynamics and Joule heating during a storm and substorm. The data from the neutral atom imager instrument can be used to study the dynamics and the energy release in the ring current region from sudden commencement to complete storm recovery. Furthermore the data from KuaFu-A, which is around L1 point, can be used to study the interplanetary conditions along with the data from the plasma sheet to study the triggering process and energy release during a substorm. So, KuaFu mission with its continuous time monitoring facilities would enable us to make much progress towards solving the underlying problems. 相似文献
502.
K. T. Lee T. Cleghorn F. Cucinotta L. Pinsky C. Zeitlin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,33(12):2211-2214
The charged particle spectrum for nuclei from protons to neon, (charge Z=10) was observed during the cruise phase and orbit around Mars by the MARIE charged particle spectrometer on the Odyssey spacecraft. The cruise data were taken between April 23, 2001 and mid-August 2001. The Mars orbit data were taken March 5, 2002 through May 2002 and are scheduled to continue until August 2004. Charge peaks are clearly separated for charges up to Z=10. Especially prominent are the carbon and oxygen peaks, with boron and nitrogen also clearly visible. Although heavy ions are much less abundant than protons in the cosmic ray environment, it is important to determine their abundances because their ionization energy losses (proportional to Z2) are far more dangerous to humans and to instruments. Thus the higher charged nuclei make a significant contribution to dose and dose equivalent received in space. Results of the charged particle spectrum measurements will be reported. 相似文献
503.
High accuracy satellite drag model (HASDM) 总被引:2,自引:0,他引:2
Mark F. Storz Bruce R. Bowman Major James I. Branson Stephen J. Casali W. Kent Tobiska 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,36(12):2497-2505
The dominant error source in force models used to predict low-perigee satellite trajectories is atmospheric drag. Errors in operational thermospheric density models cause significant errors in predicted satellite positions, since these models do not account for dynamic changes in atmospheric drag for orbit predictions. The Air Force Space Battlelab’s High Accuracy Satellite Drag Model (HASDM) estimates and predicts (out three days) a dynamically varying global density field. HASDM includes the Dynamic Calibration Atmosphere (DCA) algorithm that solves for the phases and amplitudes of the diurnal and semidiurnal variations of thermospheric density near real-time from the observed drag effects on a set of Low Earth Orbit (LEO) calibration satellites. The density correction is expressed as a function of latitude, local solar time and altitude. In HASDM, a time series prediction filter relates the extreme ultraviolet (EUV) energy index E10.7 and the geomagnetic storm index ap, to the DCA density correction parameters. The E10.7 index is generated by the SOLAR2000 model, the first full spectrum model of solar irradiance. The estimated and predicted density fields will be used operationally to significantly improve the accuracy of predicted trajectories for all low-perigee satellites. 相似文献
504.
505.
有机硅热控涂层在模拟空间环境下的原位性能 总被引:4,自引:0,他引:4
研究了热控涂层在地面模拟空间环境下的性能变化:原位测定了紫外、电子辐照过程中热控涂层的性能变化;考察了K2SiO3包覆ZnO情况对涂层性能的影响;用扫描电镜(SEM)对辐照前后涂层表面微观形貌的变化进行了观察。结果表明,无论是缩合型的硅树脂还是加成型硅橡胶,在加入ZnO填料后,耐紫外辐照的能力都有明显的提高;不同种类涂层在真空紫外辐照作用下表现出不同规律。硅酸钾包覆ZnO对于有机硅树脂和加成型硅橡胶作基料的热控涂层影响也不同。加成型硅橡胶制备得到的热控涂层有非常优异的抗电子辐照性能。 相似文献
506.
文章论述了碳化硅颗粒增强铝基(SiC_p/AL)复合材料在空间光学遥感器上的应用,较系统地介绍了已经完成的空间光学遥感器光机结构件镜身、镜盒的制造技术,并提出了对该材料在空间光学遥感器上应用前景的设想。 相似文献
507.
508.
太阳电池空间标定技术初探 总被引:1,自引:0,他引:1
随着各种新型空间太阳电池的发展和应用,在地面使用太阳模拟器对AMO标准太阳电池进行标定的方法在理论和实践上都遇到了严重的困难,最能反映其实际使用状态的空间标定成为解决问题的理想方案。国外太阳电池空间标定技术已十分成熟,主要航天国家如美国、欧洲、日本、巴西等都进行了各自的空间标定实验。北京东方计量测试研究所进行了太阳电池空间标定原理样机的研制工作。样机由太阳电池板、数据采集与处理模块、太阳敏感器和温度传感器组成,可同时对32路国产砷化镓多结太阳电池进行短路电流的测量,电流测试的标准不确定度小于0.5%(最佳点)。此项研究将形成标准太阳电池空间标定的完整方案,促进我国新型空间太阳电池的研究和应用。 相似文献
509.
510.
针对空间机械臂碰撞过程中产生的冲击和破坏问题,提出一种能被动适应碰撞且能保证操作精度的可变刚度丝驱动连续型机械臂。在以超弹镍钛合金丝为支撑脊椎和驱动部件的基础结构上,设计了一种利用温控记忆合金改变关节内摩擦力的变刚度方法。通过运动学分析得到机械臂驱动空间、构型空间和工作空间之间的坐标映射及速度雅克比矩阵,并结合末端位置反馈设计了一个稳定的闭环运动控制器。在检测丝驱动力的基础上提出了一种碰撞识别方法和相应的变刚度控制策略。运动控制和变刚度控制的实验结果表明该连续型机械臂具有良好的运动控制精度和刚度调节能力。 相似文献