全文获取类型
收费全文 | 5192篇 |
免费 | 51篇 |
国内免费 | 24篇 |
专业分类
航空 | 2429篇 |
航天技术 | 1802篇 |
综合类 | 16篇 |
航天 | 1020篇 |
出版年
2021年 | 47篇 |
2019年 | 40篇 |
2018年 | 163篇 |
2017年 | 116篇 |
2016年 | 79篇 |
2015年 | 44篇 |
2014年 | 119篇 |
2013年 | 155篇 |
2012年 | 135篇 |
2011年 | 227篇 |
2010年 | 161篇 |
2009年 | 240篇 |
2008年 | 262篇 |
2007年 | 168篇 |
2006年 | 122篇 |
2005年 | 145篇 |
2004年 | 140篇 |
2003年 | 161篇 |
2002年 | 113篇 |
2001年 | 168篇 |
2000年 | 94篇 |
1999年 | 104篇 |
1998年 | 126篇 |
1997年 | 100篇 |
1996年 | 119篇 |
1995年 | 149篇 |
1994年 | 138篇 |
1993年 | 77篇 |
1992年 | 112篇 |
1991年 | 45篇 |
1990年 | 45篇 |
1989年 | 108篇 |
1988年 | 45篇 |
1987年 | 40篇 |
1986年 | 44篇 |
1985年 | 134篇 |
1984年 | 133篇 |
1983年 | 95篇 |
1982年 | 101篇 |
1981年 | 144篇 |
1980年 | 51篇 |
1979年 | 37篇 |
1978年 | 43篇 |
1977年 | 36篇 |
1976年 | 29篇 |
1975年 | 42篇 |
1974年 | 33篇 |
1973年 | 27篇 |
1972年 | 25篇 |
1971年 | 24篇 |
排序方式: 共有5267条查询结果,搜索用时 93 毫秒
361.
A.K. Sharma D.P. Nade S.S. Nikte P.T. Patil R.N. Ghodpage R.S. Vhatkar M.V. Rokade S. Gurubaran 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
This paper reports the nightglow observations of OI 630.0 nm emissions, made by using all sky imager operating at low latitude station Kolhapur (16.8°N, 74.2°E and dip lat. 10.6°N) during high sunspot number years of 24th solar cycle. The images are analyzed to study the nocturnal, seasonal and solar activity dependence occurrence of plasma bubbles. We observed EPBs in images regularly during a limited period 19:30 to 02:30 LT and reach maximum probability of occurrence at 22:30 LT. The observation pattern of EPBs shows nearly no occurrence during the month of May and it maximizes during the period October–April. The equinox and solstice seasonal variations in the occurrence of plasma bubbles show nearly equal and large differences, respectively, between years of 2010–11 and 2011–12. 相似文献
362.
E.S. Seo T. Anderson D. Angelaszek S.J. Baek J. Baylon M. Buénerd M. Copley S. Coutu L. Derome B. Fields M. Gupta J.H. Han I.J. Howley H.G. Huh Y.S. Hwang H.J. Hyun I.S. Jeong D.H. Kah K.H. Kang D.Y. Kim H.J. Kim K.C. Kim M.H. Kim K. Kwashnak J. Lee M.H. Lee J.T. Link L. Lutz A. Malinin A. Menchaca-Rocha J.W. Mitchell S. Nutter O. Ofoha H. Park I.H. Park J.M. Park P. Patterson J.R. Smith J. Wu Y.S. Yoon 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The Cosmic Ray Energetics And Mass (CREAM) instrument is configured with a suite of particle detectors to measure TeV cosmic-ray elemental spectra from protons to iron nuclei over a wide energy range. The goal is to extend direct measurements of cosmic-ray composition to the highest energies practical, and thereby have enough overlap with ground based indirect measurements to answer questions on cosmic-ray origin, acceleration and propagation. The balloon-borne CREAM was flown successfully for about 161 days in six flights over Antarctica to measure elemental spectra of Z = 1–26 nuclei over the energy range 1010 to >1014 eV. Transforming the balloon instrument into ISS-CREAM involves identification and replacement of components that would be at risk in the International Space Station (ISS) environment, in addition to assessing safety and mission assurance concerns. The transformation process includes rigorous testing of components to reduce risks and increase survivability on the launch vehicle and operations on the ISS without negatively impacting the heritage of the successful CREAM design. The project status, including results from the ongoing analysis of existing data and, particularly, plans to increase the exposure factor by another order of magnitude utilizing the International Space Station are presented. 相似文献
363.
Analysis of the ionosphere/plasmasphere electron content variability during strong geomagnetic storm
Iu.V. Cherniak I.E. Zakharenkova D. Dzubanov A. Krankowski 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The ionosphere/plasmasphere electron content (PEC) variations during strong geomagnetic storms in November 2004 were estimated by combining of mid-latitude Kharkov incoherent scatter radar observations and GPS TEC data derived from global TEC maps. The comparison between two independent measurements was performed by analysis of the height-temporal distribution for specific location corresponding to the mid-latitudes of Europe. The percentage contribution of PEC to GPS TEC indicated the clear dependence from the time with maximal values (more than 70%) during night-time. During day-time the lesser values (30–45%) were observed for quiet geomagnetic conditions and rather high values of the PEC contribution to GPS TEC (up to 90%) were observed during strong negative storm. These changes can be explained by the competing effects of electric fields and winds, which tend to raise the layer to the region with lower loss rate and movement of the ionospheric plasma to the plasmasphere. 相似文献
364.
365.
The present paper discusses a need to develop a methodology of predicting the reliability of small thrust liquid rocket engines with a flow section made of composite materials under actual operating conditions for their successful practical use in the propulsion systems. 相似文献
366.
367.
Paul Morgan Suzanne E. Smrekar Ralph Lorenz Matthias Grott Olaf Kroemer Nils Müller 《Space Science Reviews》2017,211(1-4):277-313
The HP3 instrument on the InSight lander mission will measure subsurface temperatures and thermal conductivities from which heat flow in the upper few meters of the regolith at the landing site will be calculated. The parameter to be determined is steady-state conductive heat flow, but temperatures may have transient perturbations resulting from surface temperature changes and there could be a component of thermal convection associated with heat transport by vertical flow of atmospheric gases over the depth interval of measurement. The experiment is designed so that it should penetrate to a depth below which surface temperature perturbations are smaller than the required measurement precision by the time the measurements are made. However, if the measurements are delayed after landing, and/or the probe does not penetrate to the desired depth, corrections may be necessary for the transient perturbations. Thermal convection is calculated to be negligible, but these calculations are based on unknown physical properties of the Mars regolith. The effects of thermal convection should be apparent at shallow depths where transient thermal perturbations would be observed to deviate from conductive theory. These calculations were required during proposal review and their probability of predicting a successful measurement a prerequisite for mission approval. However, their uncertainties lies in unmeasured physical parameters of the Mars regolith. 相似文献
368.
Grasset O. Castillo-Rogez J. Guillot T. Fletcher L. N. Tosi F. 《Space Science Reviews》2017,212(1-2):835-875
Space Science Reviews - Space exploration and ground-based observations have provided outstanding evidence of the diversity and the complexity of the outer solar system. This work presents our... 相似文献
369.
为了实现航空发动机燃油喷嘴上的螺旋槽特征的快速与精确检测,提出了螺旋槽的槽深、螺旋角和槽宽等参数的测量与计算方法,并基于此设计和搭建了一套非接触式的燃油喷嘴螺旋槽精密测量系统。该测量系统基于模块化的设计思想,其机械主体采用立柱移动型三坐标测量机的结构形式;运动机构由三个直线轴X、Y和Z以及一个回转轴A构成,电气控制模块采用了由上位机与下位机构成的主从控制方式,前端传感器选用了新型的锥光偏振全息激光测头,并应用专用夹具来实现被测喷嘴零件的装夹和定位。最后,选取某个燃油喷嘴样件作为被测目标,应用所搭建的测量系统对其上的多个螺旋槽特征开展了重复测量实验,并解算得到了槽深、螺旋角和槽宽的几何尺寸,而且系统所达到的测量精度能够满足检测需求。 相似文献
370.
为了实现航空发动机燃油喷嘴上的螺旋槽特征的快速与精确检测,提出了螺旋槽的槽深、螺旋角和槽宽等参数的测量与计算方法,并基于此设计和搭建了一套非接触式的燃油喷嘴螺旋槽精密测量系统。该测量系统基于模块化的设计思想,其机械主体采用立柱移动型三坐标测量机的结构形式;运动机构由三个直线轴X、Y和Z以及一个回转轴A构成,电气控制模块采用了由上位机与下位机构成的主从控制方式,前端传感器选用了新型的锥光偏振全息激光测头,并应用专用夹具来实现被测喷嘴零件的装夹和定位。最后,选取某个燃油喷嘴样件作为被测目标,应用所搭建的测量系统对其上的多个螺旋槽特征开展了重复测量实验,并解算得到了槽深、螺旋角和槽宽的几何尺寸,而且系统所达到的测量精度能够满足检测需求。 相似文献