全文获取类型
收费全文 | 240篇 |
免费 | 36篇 |
国内免费 | 9篇 |
专业分类
航空 | 77篇 |
航天技术 | 179篇 |
综合类 | 8篇 |
航天 | 21篇 |
出版年
2024年 | 2篇 |
2023年 | 8篇 |
2022年 | 1篇 |
2021年 | 2篇 |
2020年 | 10篇 |
2019年 | 5篇 |
2018年 | 9篇 |
2017年 | 4篇 |
2016年 | 5篇 |
2015年 | 5篇 |
2014年 | 16篇 |
2013年 | 7篇 |
2012年 | 9篇 |
2011年 | 19篇 |
2010年 | 7篇 |
2009年 | 10篇 |
2008年 | 22篇 |
2007年 | 10篇 |
2006年 | 37篇 |
2005年 | 6篇 |
2004年 | 35篇 |
2003年 | 4篇 |
2002年 | 1篇 |
2001年 | 1篇 |
1999年 | 3篇 |
1998年 | 2篇 |
1997年 | 3篇 |
1996年 | 5篇 |
1995年 | 3篇 |
1994年 | 8篇 |
1993年 | 1篇 |
1992年 | 4篇 |
1988年 | 1篇 |
1987年 | 1篇 |
1984年 | 19篇 |
排序方式: 共有285条查询结果,搜索用时 15 毫秒
221.
采用XPS方法研究了卡托辛对复合固体推进剂氧化剂AP热分解过程的作用机理。结果表明,热氧化后Fe原子的结合能向高位移动,再根据Fe2p3/2谱强度的变化,说明卡托辛在AP热分解过程中是逐渐氧化过程,Fe—C共轭键逐渐断裂;Cl原子的结合能向低位移动,且在200 eV左右出现低结合能的峰,同时其强度逐渐增大,Cl原子在200 eV处形成的低结合能态的可能途径是卡托辛的分解产物环戊二烯离子与HClO4的分解产物HCl发生反应,加速了HClO4的分解速度;卡托辛的二茂铁基夹心结构破坏后生成的Fe2O3具有较高的反应活性,亦加速AP离解产物HClO4的分解速度。 相似文献
222.
Qiang Xu Xiaohu Fan Ai Gang Zhao Hongliang Cui Liguo Xu Ning Liu Bangping Ding 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):583-596
In order to shorten the data update period and further improve the accuracy, a pre-correction X-ray pulsar navigation algorithm based on asynchronous overlapping observation method is proposed. The asynchronous overlapping observation method partially overlaps the two adjacent observation periods, so that the data update period depends on the minimum pulsar observation period rather than the maximum like the other algorithms. The number of sampling points is also reduced to 2, which will effectively reduce the calculation burden. The proposed pre-correction extended Kalman filter uses observation data of adjacent sampling points to achieve a two-fold correction and makes up for the problem of insufficient observations on some sampling points caused by the observation method. Finally, simulations show that the proposed algorithm reduces the position and velocity errors by 21.55% and 19.13% compared to the EKF based on asynchronous observation method when using three detectors to observe the corresponding pulsars simultaneously. At the same time, the running time of one data update calculation is only 6.6% more than that of the EKF algorithm based on synchronous observation method. 相似文献
223.
《中国航空学报》2020,33(3):771-791
Composite materials are increasingly used in the aerospace industry. To fully realise the weight saving potential along with superior mechanical properties that composites offer in safety critical applications, reliable Non-Destructive Testing (NDT) methods are required to prevent catastrophic failures. This paper will review the state of the art in the field and point to highlight the success and challenges that different NDT methods are faced to evaluate the integrity of critical aerospace composites. The focus will be on advanced certificated NDT methods for damage detection and characterization in composite laminates for use in the aircraft primary and secondary structures. 相似文献
224.
225.
Effect of Processing and Composition on the Structure and Properties of P/M EP741NP Type Alloys 总被引:1,自引:0,他引:1
A study was carried out on the effects of processing and composition on the structure and properties of P/M EP741NP type alloys. The objectives of this study were to understand the role of Hf in a P/M superalloy containing high niobium used in aircraft engines and to determine the effects of extrusion and forging the powders as contrasted to HIPing (hot isostatic pressing) only. Two alloys of the P/M EP741NP composition were atomized: one alloy contained 0.26%Hf and the other was Hf free. After the as-atomized powders from both alloys were characterized, the powders were extruded into billets, forged and heat treated. After each process, the microstructures were characterized by SEM and the phases were extracted and identified by X-ray diffraction. The presence of Hf in the residues was probed by EDS (energy dispersive spectroscopy). The alloys were given the published Russian heat treatment as well as a more conventional heat treatment more typical of western powder alloys. Tensile, creep and stress rupture mechanical property tests were run. Results of the structural behavior of the alloys after each processing step will be presented and discussed. The role of the Hf on the mechanical proper- ties will be discussed. 相似文献
226.
S.V. Vadawale P. Sreekumar Y.B. Acharya M. Shanmugam D. Banerjee J.N. Goswami N. Bhandari C.N. Umapathy M.R. Sharma A. Tyagi M. Bug M. Sudhakar L. Abraham 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The High Energy X-ray spectrometer (HEX) on Chandrayaan-1 was designed to study the photon emission in the range of 30–270 keV from naturally occurring radioactive decay of 238U and 232Th series nuclides from the lunar surface. The primary objective of HEX was to study the transport of volatiles on the lunar surface using radon as a tracer and mapping the 46.5 keV line from 210Pb, a decay product of 222Rn. HEX was tested for two days during the commissioning phase of Chandrayaan-1 and performance of all sub systems was found to be as expected. HEX started collecting science data during the first non-prime imaging season (February–April, 2009) of Chandrayaan-1. Certain anomalies persisted in this data set and the early curtailment of Chandrayaan-1 mission in August, 2009, did not allow any further operation of HEX. Despite these issues, HEX provided the first data set for 30–270 keV continuum emission, averaged over a significant portion of the lunar surface, including the polar region. 相似文献
227.
228.
应用MonteCarlo方法对太阳X射线暴(1-8?及0.5-4?)与地球大气相互作用过程进行跟踪模拟,得到了X射线暴在电离层D层产生的电子产生率,并计算了由此产生的宇宙噪声吸收值。结果与作者在南极观测得到的X射线暴期间宇宙噪声吸收值符合较好. 相似文献
229.
构建脉冲模板是X射线脉冲星导航的一项关键技术,其精度与脉冲星角位置精度密切相关。基于脉冲模板构建的基本原理,推导得到了脉冲星角位置误差对脉冲模板构建影响的系统误差的年化平均值以及任意弧段积分的解析表达式,分析了脉冲星角位置误差对脉冲模板构建的影响。在此基础上,给出了削弱脉冲星角位置误差影响的方法。通过理论推导和仿真分析,验证了误差削弱方法的有效性,可以为优化X射线脉冲星的观测任务以及X射线脉冲模板的构建提供理论支持。 相似文献
230.
Charles E. Schlemm II Richard D. Starr George C. Ho Kathryn E. Bechtold Sarah A. Hamilton John D. Boldt William V. Boynton Walter Bradley Martin E. Fraeman Robert E. Gold John O. Goldsten John R. Hayes Stephen E. Jaskulek Egidio Rossano Robert A. Rumpf Edward D. Schaefer Kim Strohbehn Richard G. Shelton Raymond E. Thompson Jacob I. Trombka Bruce D. Williams 《Space Science Reviews》2007,131(1-4):393-415
NASA’s MESSENGER (MErcury Surface, Space ENvironment, GEochemistry, and Ranging) mission will further the understanding of
the formation of the planets by examining the least studied of the terrestrial planets, Mercury. During the one-year orbital
phase (beginning in 2011) and three earlier flybys (2008 and 2009), the X-Ray Spectrometer (XRS) onboard the MESSENGER spacecraft
will measure the surface elemental composition. XRS will measure the characteristic X-ray emissions induced on the surface
of Mercury by the incident solar flux. The Kα lines for the elements Mg, Al, Si, S, Ca, Ti, and Fe will be detected. The 12°
field-of-view of the instrument will allow a spatial resolution that ranges from 42 km at periapsis to 3200 km at apoapsis
due to the spacecraft’s highly elliptical orbit. XRS will provide elemental composition measurements covering the majority
of Mercury’s surface, as well as potential high-spatial-resolution measurements of features of interest. This paper summarizes
XRS’s science objectives, technical design, calibration, and mission observation strategy. 相似文献