首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   10093篇
  免费   658篇
  国内免费   497篇
航空   5152篇
航天技术   3068篇
综合类   446篇
航天   2582篇
  2023年   47篇
  2022年   120篇
  2021年   214篇
  2020年   133篇
  2019年   149篇
  2018年   320篇
  2017年   271篇
  2016年   227篇
  2015年   201篇
  2014年   347篇
  2013年   382篇
  2012年   405篇
  2011年   568篇
  2010年   516篇
  2009年   608篇
  2008年   575篇
  2007年   444篇
  2006年   301篇
  2005年   345篇
  2004年   267篇
  2003年   305篇
  2002年   291篇
  2001年   315篇
  2000年   229篇
  1999年   261篇
  1998年   255篇
  1997年   185篇
  1996年   231篇
  1995年   265篇
  1994年   241篇
  1993年   158篇
  1992年   187篇
  1991年   80篇
  1990年   74篇
  1989年   156篇
  1988年   77篇
  1987年   64篇
  1986年   72篇
  1985年   193篇
  1984年   149篇
  1983年   109篇
  1982年   120篇
  1981年   217篇
  1980年   51篇
  1979年   47篇
  1978年   51篇
  1977年   42篇
  1975年   50篇
  1974年   40篇
  1970年   37篇
排序方式: 共有10000条查询结果,搜索用时 776 毫秒
261.
The science payload on the Deep Impact mission includes a 1.05–4.8 μm infrared spectrometer with a spectral resolution ranging from R∼200–900. The Deep Impact IR spectrometer was designed to optimize, within engineering and cost constraints, observations of the dust, gas, and nucleus of 9P/Tempel 1. The wavelength range includes absorption and emission features from ices, silicates, organics, and many gases that are known to be, or anticipated to be, present on comets. The expected data will provide measurements at previously unseen spatial resolution before, during, and after our cratering experiment at the comet 9P/Tempel 1. This article explores the unique aspects of the Deep Impact IR spectrometer experiment, presents a range of expectations for spectral data of 9P/Tempel 1, and summarizes the specific science objectives at each phase of the mission.  相似文献   
262.
In 1998, Comet 9P/Tempel 1 was chosen as the target of the Deep Impact mission (A’Hearn, M. F., Belton, M. J. S., and Delamere, A., Space Sci. Rev., 2005) even though very little was known about its physical properties. Efforts were immediately begun to improve this situation by the Deep Impact Science Team leading to the founding of a worldwide observing campaign (Meech et al., Space Sci. Rev., 2005a). This campaign has already produced a great deal of information on the global properties of the comet’s nucleus (summarized in Table I) that is vital to the planning and the assessment of the chances of success at the impact and encounter. Since the mission was begun the successful encounters of the Deep Space 1 spacecraft at Comet 19P/Borrelly and the Stardust spacecraft at Comet 81P/Wild 2 have occurred yielding new information on the state of the nuclei of these two comets. This information, together with earlier results on the nucleus of comet 1P/Halley from the European Space Agency’s Giotto, the Soviet Vega mission, and various ground-based observational and theoretical studies, is used as a basis for conjectures on the morphological, geological, mechanical, and compositional properties of the surface and subsurface that Deep Impact may find at 9P/Tempel 1. We adopt the following working values (circa December 2004) for the nucleus parameters of prime importance to Deep Impact as follows: mean effective radius = 3.25± 0.2 km, shape – irregular triaxial ellipsoid with a/b = 3.2± 0.4 and overall dimensions of ∼14.4 × 4.4 × 4.4 km, principal axis rotation with period = 41.85± 0.1 hr, pole directions (RA, Dec, J2000) = 46± 10, 73± 10 deg (Pole 1) or 287± 14, 16.5± 10 deg (Pole 2) (the two poles are photometrically, but not geometrically, equivalent), Kron-Cousins (V-R) color = 0.56± 0.02, V-band geometric albedo = 0.04± 0.01, R-band geometric albedo = 0.05± 0.01, R-band H(1,1,0) = 14.441± 0.067, and mass ∼7×1013 kg assuming a bulk density of 500 kg m−3. As these are working values, {i.e.}, based on preliminary analyses, it is expected that adjustments to their values may be made before encounter as improved estimates become available through further analysis of the large database being made available by the Deep Impact observing campaign. Given the parameters listed above the impact will occur in an environment where the local gravity is estimated at 0.027–0.04 cm s−2 and the escape velocity between 1.4 and 2 m s−1. For both of the rotation poles found here, the Deep Impact spacecraft on approach to encounter will find the rotation axis close to the plane of the sky (aspect angles 82.2 and 69.7 deg. for pole 1 and 2, respectively). However, until the rotation period estimate is substantially improved, it will remain uncertain whether the impactor will collide with the broadside or the ends of the nucleus.  相似文献   
263.
电磁兼容技术   总被引:11,自引:0,他引:11  
介绍了电磁兼容技术的产生及其发展现状 ,重点介绍了当前的电磁兼容预测技术以及工程实现电磁兼容的主要方法。探讨了电磁兼容领域面临的问题以及当前的主要研究方向。  相似文献   
264.
赵一鹗  余少志 《推进技术》1996,17(6):40-42,68
用按物理过程作时间分裂的无粘-粘性分数步法求解可压缩N-S方程,无粘步用高效欧拉算法解欧拉方程,粘性步用全隐格式解抛物方程;并采取了有效措施消除由分步法产生的时间和空间不相容性,文中给出了轴对称喷管内外流场的数值模拟结果。  相似文献   
265.
研究了降低浇注温度或加入细化剂后 ,K4 16 9合金晶粒细化的微观组织、夹杂及缩松等的变化。发现同样加或不加细化剂条件下 ,浇注温度越低 ,一次枝晶主轴长度和二次枝晶臂距越小。而同一浇注温度下 ,化学法细晶试样一次枝晶主轴长度较普通试样的短 ,而二者的二次枝晶臂距无明显差别。晶粒细化后 ,晶粒形态由普通铸造组织中的树枝晶向细晶组织中的粒状晶转变 ,且合金中主要元素的偏析减轻 ,这均有利于提高细晶铸件机械性能。MC型碳化物和Laves相的尺寸、数量和形貌在晶粒细化前后变化不大。铸件中加入微量细化剂不形成夹杂 ,不改变合金相组成。此外 ,加细化剂不仅可使晶粒细化 ,同时铸件中的缩松大大减少  相似文献   
266.
It is shown that the errors associated with radio elevation measurements may be investigated systematically using a variational technique. The error occurring when spaced antennas are used is compared with that for a single directional antenna. Integral expressions are obtained for the refractive errors.  相似文献   
267.
Present-Day Sea Level Change: Observations and Causes   总被引:3,自引:0,他引:3  
Cazenave  A.  Cabanes  C.  Dominh  K.  Gennero  M.C.  Le Provost  C. 《Space Science Reviews》2003,108(1-2):131-144
We investigate climate-related processes causing variations of the global mean sea level on interannual to decadal time scale. We focus on thermal expansion of the oceans and continental water mass balance. We show that during the 1990s where global mean sea level change has been measured by Topex/Poseidon satellite altimetry, thermal expansion is the dominant contribution to the observed 2.5 mm/yr sea level rise. For the past decades, exchange of water between continental reservoirs and oceans had a small, but not totally negligible contribution (about 0.2 mm/yr) to sea level rise. For the last four decades, thermal contribution is estimated to about 0.5 mm/yr, with a possible accelerated rate of thermosteric rise during the 1990s. Topex/Poseidon shows an increase in mean sea level of 2.5 mm/yr over the last decade, a value about two times larger than reported by historical tide gauges. This would suggest that there has been significant acceleration of sea level rise in the recent past, possibly related to ocean warming. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
268.
Jurewicz  A.J.G.  Burnett  D.S.  Wiens  R.C.  Friedmann  T.A.  Hays  C.C.  Hohlfelder  R.J.  Nishiizumi  K.  Stone  J.A.  Woolum  D.S.  Becker  R.  Butterworth  A.L.  Campbell  A.J.  Ebihara  M.  Franchi  I.A.  Heber  V.  Hohenberg  C.M.  Humayun  M.  McKeegan  K.D.  McNamara  K.  Meshik  A.  Pepin  R.O.  Schlutter  D.  Wieler  R. 《Space Science Reviews》2003,105(3-4):535-560
Genesis (NASA Discovery Mission #5) is a sample return mission. Collectors comprised of ultra-high purity materials will be exposed to the solar wind and then returned to Earth for laboratory analysis. There is a suite of fifteen types of ultra-pure materials distributed among several locations. Most of the materials are mounted on deployable panels (‘collector arrays’), with some as targets in the focal spot of an electrostatic mirror (the ‘concentrator’). Other materials are strategically placed on the spacecraft as additional targets of opportunity to maximize the area for solar-wind collection. Most of the collection area consists of hexagonal collectors in the arrays; approximately half are silicon, the rest are for solar-wind components not retained and/or not easily measured in silicon. There are a variety of materials both in collector arrays and elsewhere targeted for the analyses of specific solar-wind components. Engineering and science factors drove the selection process. Engineering required testing of physical properties such as the ability to withstand shaking on launch and thermal cycling during deployment. Science constraints included bulk purity, surface and interface cleanliness, retentiveness with respect to individual solar-wind components, and availability. A detailed report of material parameters planned as a resource for choosing materials for study will be published on a Genesis website, and will be updated as additional information is obtained. Some material is already linked to the Genesis plasma data website (genesis.lanl.gov). Genesis should provide a reservoir of materials for allocation to the scientific community throughout the 21st Century. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
269.
Schunker  H.  Donea  A. -C. 《Space Science Reviews》2003,107(1-2):99-102
We present preliminary results from high resolution observations obtained with the Michelson Doppler Imager (MDI) instrument on the SOHO of two large solar flares of 14 July 2000 and 24 November 2000. We show that rapid variations of the line-of-sight magnetic field occured on a time scale of a few minutes during the flare explosions. The reversibility/irreversibility of the magnetic field of both active regions is a very good tool for understanding how the magnetic energy is released in these flares. The observed sharp increase of the magnetic energy density at the time of maximum of the solar flare could involve an unknown component which deposited supplementary energy into the system. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
270.
Spectral-domain covariance estimation with a priori knowledge   总被引:2,自引:0,他引:2  
A knowledge-aided spectral-domain approach to estimating the interference covariance matrix used in space-time adaptive processing (STAP) is proposed. Prior knowledge of the range-Doppler clutter scene is used to identify geographic regions with homogeneous scattering statistics. Then, minimum-variance spectral estimation is used to arrive at a spectral-domain clutter estimate. Finally, space-time steering vectors are used to transform the spectral-domain estimate into a data-domain estimate of the clutter covariance matrix. The proposed technique is compared with ideal performance and to the fast maximum likelihood technique using simulated results. An investigation of the performance degradation that can occur due to various inaccurate knowledge assumptions is also presented  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号