全文获取类型
收费全文 | 227篇 |
免费 | 28篇 |
国内免费 | 5篇 |
专业分类
航空 | 43篇 |
航天技术 | 157篇 |
航天 | 60篇 |
出版年
2023年 | 5篇 |
2021年 | 7篇 |
2020年 | 6篇 |
2019年 | 4篇 |
2018年 | 8篇 |
2017年 | 1篇 |
2016年 | 2篇 |
2015年 | 6篇 |
2014年 | 15篇 |
2013年 | 13篇 |
2012年 | 18篇 |
2011年 | 23篇 |
2010年 | 16篇 |
2009年 | 16篇 |
2008年 | 19篇 |
2007年 | 5篇 |
2006年 | 8篇 |
2005年 | 9篇 |
2004年 | 3篇 |
2003年 | 4篇 |
2002年 | 6篇 |
2001年 | 7篇 |
2000年 | 4篇 |
1999年 | 2篇 |
1998年 | 7篇 |
1996年 | 3篇 |
1995年 | 6篇 |
1994年 | 4篇 |
1993年 | 10篇 |
1992年 | 8篇 |
1991年 | 3篇 |
1990年 | 3篇 |
1989年 | 1篇 |
1988年 | 5篇 |
1987年 | 1篇 |
1984年 | 2篇 |
排序方式: 共有260条查询结果,搜索用时 250 毫秒
111.
空间的高能重离子和高能质子都能引起单粒子效应。几种典型环境中的重离子和质子对不同器件单粒子效应的影响的比较表明,在地磁捕获质子强度较大的区域,捕获质子对单粒子效应的作用必须考虑;而在该区域以外,对单粒子效应的发生有显著影响的是宇宙射线的重离子而不是占绝大多数的质子。 相似文献
112.
辐射发射与辐射法测温—如何接近表面真实温度 总被引:1,自引:0,他引:1
从辐射测法中辐射率变化对温度的影响,讨论了多色辐射测量法的发展与应用实践,比较了不同处理方法的优缺点。 相似文献
113.
B.C. Joshi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2006,38(12):2725-2727
The double pulsar system, J0737–3039, provides a unique probe of a pulsar magnetosphere due to its edge-on viewing geometry, a tight orbit and a significant rate of advance of the angle of periastron. In this paper, we report on the changes in radio emission from the long period pulsar in this system, J0737–3039B, over a period of 9 months. Observations of this system with Giant Metrewave Radio Telescope (GMRT) show that the duration of the first bright phase of the pulsar centered at 210° orbital longitude from the ascending node is shrinking. These observations will be useful to constrain the proposed models for this system. 相似文献
114.
115.
116.
117.
G. Bazzano A. Ampollini F. Cardelli F. Fortini P. Nenzi G.B. Palmerini L. Picardi L. Piersanti C. Ronsivalle V. Surrenti E. Trinca M. Vadrucci M. Sabatini 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(4):1379-1391
We present the first results of a novel collaboration activity between ENEA Frascati Particle Accelerator Laboratory and University La Sapienza Guidance and Navigation Laboratory in the field of Radiation Hardness Assurance (RHA) for space applications.The aim of this research is twofold: (a) demonstrating the possibility to use the TOP-IMPLART proton accelerator for radiation hardness assurance testing, developing ad hoc dosimetric and operational procedures for RHA irradiations; (b) investigating system level radiation testing strategies for Commercial Off The Shelf (COTS) components of interest for SmallSats space missions, with focus on devices and sensors of interest for guidance, navigation and control, through simultaneous exploration of Total Ionizing Dose (TID), Displacement Damage (DD) dose and Single-Event Effects (SEE) with proton beams.A commercial 6-axis integrated Micro Electro-Mechanical Systems (MEMS) inertial navigation system (accelerometer, gyroscope) was selected as first Device Under Test (DUT). The results of experimental tests aimed to define an operational procedure and the characterization of radiation effects on the component are reported, highlighting the consequence of the device performance degradation in terms of the overall navigation system accuracy. Doses up to 50 krad(Si) were probed and cross sections for Single-Event Functional Interrupt (SEFI) evaluated at a proton energy of 30 MeV. 相似文献
118.
Xiujie Jiang Zhihua Wang Huixian Sun Xiaomin Chen Tianlin Zhao Guanghua Yu Changyi Zhou 《Acta Astronautica》2009,65(9-10):1500-1505
More and more plastic encapsulated microcircuits (PEMs) are used in space missions to achieve high performance. Since PEMs are designed for use in terrestrial operating conditions, the successful usage of PEMs in space harsh environment is closely related to reliability issues, which should be considered firstly. However, there is no ready-made methodology for PEMs in space applications. This paper discusses the reliability for the usage of PEMs in space. This reliability analysis can be divided into five categories: radiation test, radiation hardness, screening test, reliability calculation and reliability assessment. One case study is also presented to illuminate the details of the process, in which a PEM part is used in a joint space program Double-Star Project between the European Space Agency (ESA) and China. The influence of environmental constrains including radiation, humidity, temperature and mechanics on the PEM part has been considered. Both Double-Star Project satellites are still running well in space now. 相似文献
119.
S. Valk A. Lemaître L. Anselmo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(7):1077-1090
This paper provides a Hamiltonian formulation of the averaged equations of motion with respect to short periods (1 day) of a space debris subjected to direct solar radiation pressure and orbiting near the geostationary ring. This theory is based on a semi-analytical theory of order 1 regarding the averaging process, formulated using canonical and non-singular elements for eccentricity and inclination. The analysis is based on an expansion in powers of the eccentricity and of the inclination, truncated at an arbitrary high order. 相似文献
120.
J. S. Kaastra F. B. S. Paerels F. Durret S. Schindler P. Richter 《Space Science Reviews》2008,134(1-4):155-190
We discuss the different physical processes that are important to understand the thermal X-ray emission and absorption spectra
of the diffuse gas in clusters of galaxies and the warm-hot intergalactic medium. The ionisation balance, line and continuum
emission and absorption properties are reviewed and several practical examples are given that illustrate the most important
diagnostic features in the X-ray spectra. 相似文献