全文获取类型
收费全文 | 7821篇 |
免费 | 50篇 |
国内免费 | 41篇 |
专业分类
航空 | 3938篇 |
航天技术 | 2759篇 |
综合类 | 92篇 |
航天 | 1123篇 |
出版年
2021年 | 56篇 |
2018年 | 87篇 |
2017年 | 79篇 |
2016年 | 51篇 |
2014年 | 138篇 |
2013年 | 201篇 |
2012年 | 168篇 |
2011年 | 276篇 |
2010年 | 204篇 |
2009年 | 282篇 |
2008年 | 371篇 |
2007年 | 213篇 |
2006年 | 218篇 |
2005年 | 220篇 |
2004年 | 161篇 |
2003年 | 243篇 |
2002年 | 159篇 |
2001年 | 249篇 |
2000年 | 170篇 |
1999年 | 207篇 |
1998年 | 225篇 |
1997年 | 177篇 |
1996年 | 218篇 |
1995年 | 257篇 |
1994年 | 242篇 |
1993年 | 151篇 |
1992年 | 174篇 |
1991年 | 98篇 |
1990年 | 94篇 |
1989年 | 191篇 |
1988年 | 89篇 |
1987年 | 84篇 |
1986年 | 87篇 |
1985年 | 249篇 |
1984年 | 201篇 |
1983年 | 173篇 |
1982年 | 172篇 |
1981年 | 242篇 |
1980年 | 78篇 |
1979年 | 58篇 |
1978年 | 73篇 |
1977年 | 69篇 |
1976年 | 55篇 |
1975年 | 84篇 |
1974年 | 53篇 |
1973年 | 54篇 |
1972年 | 74篇 |
1971年 | 57篇 |
1970年 | 55篇 |
1969年 | 52篇 |
排序方式: 共有7912条查询结果,搜索用时 520 毫秒
641.
G. L. Gdalevich N. I. Izhovkina V. D. Ozerov N. Bankov S. Chapkanov L. Todorieva 《Cosmic Research》2006,44(5):419-424
The results of the satellite low-latitude and mid-latitude measurements of the disturbed plasma concentration, electron temperature, and quasi-stable electric field at heights of ~900 km after sunset are discussed. It is shown that the sharp fronts of changes in the electron temperature and plasma density observed in the experiment onboard the Intercosmos-Bulgaria-1300 satellite in the low-latitude (and equatorial) outer ionosphere can be related to damping of the oscillations of plasma electrons at local decreases of the plasma density (plasma “pits”) and formation of the vortex plasma structures at density and temperature gradients, which promotes conservation of ionosphere irregularities and makes the fronts of concentration variations steeper. Nonmonotonic variations in the plasma conductivity for the ionosphere currents in unstable plasma can be a cause of observed nonmonotonic disturbances of the vertical component of the “constant” electric field. 相似文献
642.
643.
A.?I.?EfimovEmail author L.?A.?Lukanina I.?V.?Chashei S.?F.?Kolomiets M.?K.?Bird M.?P?tzold 《Cosmic Research》2018,56(1):1-10
In 2013 and 2015, investigations of the internal solar wind were carried out using the method of two-frequency radio sounding by signals from the Mars Express European spacecraft. The values of the S- and X-bands’ frequency and the differential frequency were registered with a sampling rate of 1s at the American and European networks of ground-based tracking stations. The spatial distribution of the frequency fluctuation’s level has been studied. It has been shown that the intensity of frequency fluctuation considerably decreases at high heliolatitudes. In some radio sounding sessions, quasiperiodic oscillations of sub-mHz band have been observed in the temporal spectra of frequency fluctuations; they are supposed to be associated with the density inhomogeneities, the sizes of which are close to the turbulence outer scale. 相似文献
644.
Soviet General Secretary Gorbachev has proposed a joint US-Soviet programme to explore the planet Mars. The authors argue that there is considerable advantage to be gained from such a programme for both countries and for all nations on Earth. They trace the history of the US and Soviet space programmes and of cooperation between the two nations, focusing particularly on activities relating to Mars. Robotic Mars exploration is already technically possible and could take place in the 1990s, and a first step towards manned exploration could be the writing of a development and flight plan aiming for the first decade of the 21st century. 相似文献
645.
Stephen J. Pyne 《Space Policy》1988,4(3)
The world has known three great ages of exploration-the circumnavigation of the globe, with its attendant discovery of new lands; the traversing and cataloguing of the newly-found continents; and the exploration of the uninhabited regions of Antarctica, the deep ocean basins and outer space. The author points to the culturally and historically determined nature of discovery, which has thus far been largely a Western phenomenon, but emphasizes the qualitatively different character of space which takes the Earth, rather than any particular part of it, as its starting point, and which sets forth to chart regions that are most probably abiotic. 相似文献
646.
F. Bagenal A. Adriani F. Allegrini S. J. Bolton B. Bonfond E. J. Bunce J. E. P. Connerney S. W. H. Cowley R. W. Ebert G. R. Gladstone C. J. Hansen W. S. Kurth S. M. Levin B. H. Mauk D. J. McComas C. P. Paranicas D. Santos-Costa R. M. Thorne P. Valek J. H. Waite P. Zarka 《Space Science Reviews》2017,213(1-4):219-287
In July 2016, NASA’s Juno mission becomes the first spacecraft to enter polar orbit of Jupiter and venture deep into unexplored polar territories of the magnetosphere. Focusing on these polar regions, we review current understanding of the structure and dynamics of the magnetosphere and summarize the outstanding issues. The Juno mission profile involves (a) a several-week approach from the dawn side of Jupiter’s magnetosphere, with an orbit-insertion maneuver on July 6, 2016; (b) a 107-day capture orbit, also on the dawn flank; and (c) a series of thirty 11-day science orbits with the spacecraft flying over Jupiter’s poles and ducking under the radiation belts. We show how Juno’s view of the magnetosphere evolves over the year of science orbits. The Juno spacecraft carries a range of instruments that take particles and fields measurements, remote sensing observations of auroral emissions at UV, visible, IR and radio wavelengths, and detect microwave emission from Jupiter’s radiation belts. We summarize how these Juno measurements address issues of auroral processes, microphysical plasma physics, ionosphere-magnetosphere and satellite-magnetosphere coupling, sources and sinks of plasma, the radiation belts, and the dynamics of the outer magnetosphere. To reach Jupiter, the Juno spacecraft passed close to the Earth on October 9, 2013, gaining the necessary energy to get to Jupiter. The Earth flyby provided an opportunity to test Juno’s instrumentation as well as take scientific data in the terrestrial magnetosphere, in conjunction with ground-based and Earth-orbiting assets. 相似文献
647.
S. B. Mende H. U. Frey K. Rider C. Chou S. E. Harris O. H. W. Siegmund S. L. England C. Wilkins W. Craig T. J. Immel P. Turin N. Darling J. Loicq P. Blain E. Syrstad B. Thompson R. Burt J. Champagne P. Sevilla S. Ellis 《Space Science Reviews》2017,212(1-2):655-696
ICON Far UltraViolet (FUV) imager contributes to the ICON science objectives by providing remote sensing measurements of the daytime and nighttime atmosphere/ionosphere. During sunlit atmospheric conditions, ICON FUV images the limb altitude profile in the shortwave (SW) band at 135.6 nm and the longwave (LW) band at 157 nm perpendicular to the satellite motion to retrieve the atmospheric O/N2 ratio. In conditions of atmospheric darkness, ICON FUV measures the 135.6 nm recombination emission of \(\mathrm{O}^{+}\) ions used to compute the nighttime ionospheric altitude distribution. ICON Far UltraViolet (FUV) imager is a Czerny–Turner design Spectrographic Imager with two exit slits and corresponding back imager cameras that produce two independent images in separate wavelength bands on two detectors. All observations will be processed as limb altitude profiles. In addition, the ionospheric 135.6 nm data will be processed as longitude and latitude spatial maps to obtain images of ion distributions around regions of equatorial spread F. The ICON FUV optic axis is pointed 20 degrees below local horizontal and has a steering mirror that allows the field of view to be steered up to 30 degrees forward and aft, to keep the local magnetic meridian in the field of view. The detectors are micro channel plate (MCP) intensified FUV tubes with the phosphor fiber-optically coupled to Charge Coupled Devices (CCDs). The dual stack MCP-s amplify the photoelectron signals to overcome the CCD noise and the rapidly scanned frames are co-added to digitally create 12-second integrated images. Digital on-board signal processing is used to compensate for geometric distortion and satellite motion and to achieve data compression. The instrument was originally aligned in visible light by using a special grating and visible cameras. Final alignment, functional and environmental testing and calibration were performed in a large vacuum chamber with a UV source. The test and calibration program showed that ICON FUV meets its design requirements and is ready to be launched on the ICON spacecraft. 相似文献
648.
In the 1990s, based on detailed studies of the structure of active regions (AR), the concept of the magnetosphere of the active region was proposed. This includes almost all known structures presented in the active region, ranging from the radio granulation up to noise storms, the radiation of which manifests on the radio waves. The magnetosphere concept, which, from a common point of view, considers the manifestations of the radio emission of the active region as a single active complex, allows one to shed light on the relation between stable and active processes and their interrelations. It is especially important to identify the basic ways of transforming nonthermal energy into thermal energy. A dominant role in all processes is attributed to the magnetic field, the measurement of which on the coronal levels can be performed by radio-astronomical techniques. The extension of the wavelength range and the introduction of new tools and advanced modeling capabilities makes it possible to analyze the physical properties of plasma structures in the AR magnetosphere and to evaluate the coronal magnetic fields at the levels of the chromosphere–corona transition zone and the lower corona. The features and characteristics of the transition region from the S component to the B component have been estimated. 相似文献
649.
Rain.L 《中国航天(英文版)》2008,(1)
THE FOURTH BEIDOU NAVIGATION EXPERIMENTAL SATELLITE LAUNCHED The fourth Beidou experimental navigation satellite was launched into snace aton a LM-3A launch vehicle at Xichang Satellite Launch Center on February 3 at 00:28(Beijing Time).24 minutes later,the satellite separated from the launch vehicle and 相似文献
650.
Rain.L 《中国航天(英文版)》2008,(2)
FY-3A,the first satellite of China's new generation of polar-orbiting meteorological satellites,was launched into space atop a modified LM-4C launch vehicle.The satellite separated from the rocket 19 minutes after the takeoff.Flying at an altitude of 807km with an inclination of 98.8 degrees,the satellite circles in polar orbit 14 times everyday,covering the whole globe twice a day. FY-3A has a design lifetime of three years.Weighing 2295kg,the three-axis stabilized satellite is equipped with 11 remote s... 相似文献