全文获取类型
收费全文 | 7181篇 |
免费 | 6篇 |
国内免费 | 17篇 |
专业分类
航空 | 3484篇 |
航天技术 | 2124篇 |
综合类 | 189篇 |
航天 | 1407篇 |
出版年
2021年 | 48篇 |
2018年 | 208篇 |
2017年 | 160篇 |
2016年 | 106篇 |
2015年 | 45篇 |
2014年 | 130篇 |
2013年 | 152篇 |
2012年 | 180篇 |
2011年 | 328篇 |
2010年 | 243篇 |
2009年 | 360篇 |
2008年 | 360篇 |
2007年 | 266篇 |
2006年 | 130篇 |
2005年 | 175篇 |
2004年 | 178篇 |
2003年 | 206篇 |
2002年 | 223篇 |
2001年 | 277篇 |
2000年 | 125篇 |
1999年 | 147篇 |
1998年 | 187篇 |
1997年 | 122篇 |
1996年 | 170篇 |
1995年 | 202篇 |
1994年 | 173篇 |
1993年 | 110篇 |
1992年 | 151篇 |
1991年 | 65篇 |
1990年 | 72篇 |
1989年 | 151篇 |
1988年 | 66篇 |
1987年 | 73篇 |
1986年 | 65篇 |
1985年 | 194篇 |
1984年 | 147篇 |
1983年 | 128篇 |
1982年 | 147篇 |
1981年 | 206篇 |
1980年 | 71篇 |
1979年 | 52篇 |
1978年 | 64篇 |
1977年 | 47篇 |
1976年 | 49篇 |
1975年 | 58篇 |
1974年 | 52篇 |
1972年 | 51篇 |
1971年 | 50篇 |
1970年 | 33篇 |
1969年 | 35篇 |
排序方式: 共有7204条查询结果,搜索用时 31 毫秒
801.
802.
A. I. Efimov L. A. Lukanina V. K. Rudash L. N. Samoznaev I. V. Chashei M. K. Bird M. Pätzold 《Cosmic Research》2013,51(1):13-22
We have performed spectral processing of the data of experiments on radio sounding of circumsolar plasma by coherent S- and X-band signals from the spacecraft Ulysses, Mars Express, Rosetta, and Venus Express carried out from 1991 to 2009. The experiments were realized in the mode of coherent response, when a signal stabilized by the hydrogen standard is transmitted from the ground station to a spacecraft, received by the onboard systems, and retransmitted to the Earth with conserved coherence. Thus, the signal sounding the coronal plasma passes twice through the medium: on the propagation path ground station — spacecraft and on the same path in the opposite direction. The spectra of frequency fluctuations in both the bands are obtained and, using them, the radial dependences of fluctuation intensities are found, which can be approximated by a power law. It is shown that the ratio of intensities of frequency fluctuations in the S- and X-bands is comparable with the theoretical value and characterizes the degree of correlation of irregularities of the electron density along the propagation path ground station — spacecraft and back. Analysis of the correlation of frequency fluctuations on the two paths allows one to get a lower estimate of the outer scale of the circumsolar plasma turbulence. For heliocentric distances R = 10 solar radii (R S ) the outer scale is larger than 0.25R S . 相似文献
803.
Robert A. Goehlich Jay K. AndersonNathan N. Harrold Joseph A. BemisMike T. Nettleingham Joshua M. CobinBradley R. Zimmerman Ben L. AvniMichael D. Gonyea Nicholas Y. Ilchena 《Space Policy》2013
This article sheds light on the key player needed for any space tourism adventure: the pilot who flies the spacecraft. The paper addresses the potential benefits of including a pilot at the controls when designing a space tourism spacecraft. It examines the basic qualifications and advanced skills required of space tourism pilots and discusses key training requirements for selected pilots and space pilots' pay and benefits. In addition, the research concludes that, just as the pioneers of passenger transport in aviation entertained and captured the interest of their passengers, the space pilot should have the skills of a tour guide. 相似文献
804.
Deborah L. Domingue Clark R. Chapman Rosemary M. Killen Thomas H. Zurbuchen Jason A. Gilbert Menelaos Sarantos Mehdi Benna James A. Slavin David Schriver Pavel M. Trávníček Thomas M. Orlando Ann L. Sprague David T. Blewett Jeffrey J. Gillis-Davis William C. Feldman David J. Lawrence George C. Ho Denton S. Ebel Larry R. Nittler Faith Vilas Carle M. Pieters Sean C. Solomon Catherine L. Johnson Reka M. Winslow Jörn Helbert Patrick N. Peplowski Shoshana Z. Weider Nelly Mouawad Noam R. Izenberg William E. McClintock 《Space Science Reviews》2014,181(1-4):121-214
Mercury’s regolith, derived from the crustal bedrock, has been altered by a set of space weathering processes. Before we can interpret crustal composition, it is necessary to understand the nature of these surface alterations. The processes that space weather the surface are the same as those that form Mercury’s exosphere (micrometeoroid flux and solar wind interactions) and are moderated by the local space environment and the presence of a global magnetic field. To comprehend how space weathering acts on Mercury’s regolith, an understanding is needed of how contributing processes act as an interactive system. As no direct information (e.g., from returned samples) is available about how the system of space weathering affects Mercury’s regolith, we use as a basis for comparison the current understanding of these same processes on lunar and asteroidal regoliths as well as laboratory simulations. These comparisons suggest that Mercury’s regolith is overturned more frequently (though the characteristic surface time for a grain is unknown even relative to the lunar case), more than an order of magnitude more melt and vapor per unit time and unit area is produced by impact processes than on the Moon (creating a higher glass content via grain coatings and agglutinates), the degree of surface irradiation is comparable to or greater than that on the Moon, and photon irradiation is up to an order of magnitude greater (creating amorphous grain rims, chemically reducing the upper layers of grains to produce nanometer-scale particles of metallic iron, and depleting surface grains in volatile elements and alkali metals). The processes that chemically reduce the surface and produce nanometer-scale particles on Mercury are suggested to be more effective than similar processes on the Moon. Estimated abundances of nanometer-scale particles can account for Mercury’s dark surface relative to that of the Moon without requiring macroscopic grains of opaque minerals. The presence of nanometer-scale particles may also account for Mercury’s relatively featureless visible–near-infrared reflectance spectra. Characteristics of material returned from asteroid 25143 Itokawa demonstrate that this nanometer-scale material need not be pure iron, raising the possibility that the nanometer-scale material on Mercury may have a composition different from iron metal [such as (Fe,Mg)S]. The expected depletion of volatiles and particularly alkali metals from solar-wind interaction processes are inconsistent with the detection of sodium, potassium, and sulfur within the regolith. One plausible explanation invokes a larger fine fraction (grain size <45 μm) and more radiation-damaged grains than in the lunar surface material to create a regolith that is a more efficient reservoir for these volatiles. By this view the volatile elements detected are present not only within the grain structures, but also as adsorbates within the regolith and deposits on the surfaces of the regolith grains. The comparisons with findings from the Moon and asteroids provide a basis for predicting how compositional modifications induced by space weathering have affected Mercury’s surface composition. 相似文献
805.
Coronal holes are the coolest and darkest regions of the upper solar atmosphere, as observed both on the solar disk and above the solar limb. Coronal holes are associated with rapidly expanding open magnetic fields and the acceleration of the high-speed solar wind. During the years of the solar minima, coronal holes are generally confined to the Sun??s polar regions, while at solar maxima they can also be found at lower latitudes. Waves, observed via remote sensing and detected in-situ in the wind streams, are most likely responsible for the wind and several theoretical models describe the role of MHD waves in the acceleration of the fast solar wind. This paper reviews the observational evidences of detection of propagating waves in these regions. The characteristics of the waves, like periodicities, amplitude, speed provide input parameters and also act as constraints on theoretical models of coronal heating and solar wind acceleration. 相似文献
806.
Dynamics of a satellite-stabilizer system is studied. It is supposed that there is a viscous friction in a hinge connecting
two bodies, but there is no elasticity. The attitude motion in a plane of circular orbit is considered, and parameters are
determined, at which natural oscillations near a stable equilibrium position in the orbital coordinate system are damped out
most rapidly. The rate of transient processes is estimated by a value of the degree of stability of linearized equations of
motion. The optimization of the degree of stability is sequentially performed in dimensionless damping coefficient (the first
stage) and in inertial system parameters (the second stage). The result of the first stage is the partition of system parameter
space into the regions, in each of which the maximum of the degree of stability is reached on a particular configuration of
roots of the characteristic equation. It is shown at the second stage that the global maximum is reached at two points of
parameter space, where one of system bodies degenerates into a plate, and the characteristic equation has four equal real
roots. 相似文献
807.
Ovshinsky S.R. Dhar S.K. Fetcenko M.A. Corrigan D.A. Reichman B. Young K. Fierro C. Venkatesan S. Gifford P. Koch J. 《Aerospace and Electronic Systems Magazine, IEEE》1999,14(5):17-23
While Ovonic NiMH batteries are already in high volume commercial production for portable applications, advances in materials technology have enabled performance improvements in specific energy (100 Wh/kg), specific power (600-1000 W/kg), high temperature operation, charge retention, and voltage stability. Concurrent with technology advances, Ovonic NiMH batteries have established performance and commercial milestones in electric vehicles, hybrid electric vehicles, as well as scooter, motorcycle and bicycle applications. As important as these advances, significant manufacturing cost reductions have also occurred which allow continued growth of NiMH technology. In this paper, advances in performance, applications and cost reduction are discussed with particular emphasis on the improved proprietary metal hydride and nickel hydroxide materials that make such advances possible 相似文献
808.
The past dozen years have produced a new paradigm with regard to the source regions of comets in the early solar system. It
is now widely recognized that the likely source of the Jupiter-family short-period comets (those with Tisserand parameters,
T > 2 and periods, P, generally < 20 years) is the Kuiper belt in the ecliptic plane beyond Neptune. In contrast, the source
of the Halley-type and long-period comets (those with T < 2 and P > 20 years) appears to be the Oort cloud. However, the comets
in the Oort cloud almost certainly originated elsewhere, since accretion is very inefficient at such large heliocentric distances.
New dynamical studies now suggest that the source of the Oort cloud comets is the entire giant planets region from Jupiter
to Neptune, rather than primarily the Uranus-Neptune region, as previously thought. Some fraction of the Oort cloud population
may even be asteroidal bodies formed inside the orbit of Jupiter. These comets and asteroids underwent a complex dynamical
random walk among the giant planets before they were ejected to distant orbits in the Oort cloud, with possible interesting
consequences for their thermal and collisional histories. Observational evidence for diversity in cometary compositions is
limited, at best.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
809.
Castella F.R. Dunnebacke F.G. 《IEEE transactions on aerospace and electronic systems》1974,(6):891-895
A two-dimensional x, y Kalman tracking filter is analyzed for a track-while-scan (TWS) operation when the radar sensor measures range and bearing (r, ?) at uniform sampling intervals T seconds apart. This development explicitly considers the coupling between the quantities measured by the sensor (r, ?) and the Cartesian x, y coordinate system selected for the tracking operation. The steadystate components of the gain and error covariance matrixes are analytically determined under the assumption of a white noise maneuver acceleration model in two dimensions. These results are verified by computer calculation of the Kalman filter matrix equations. 相似文献
810.
Robbins Earl R. Moody Douglas E. Happ William W. 《IEEE transactions on aerospace and electronic systems》1966,(4):370-375
Flowgraph techniques are extended to systems with piecewise-linear characteristics by developing criteria for construction of an optimum model from related subregions in which linearity holds. This requires the synthesis of several known techniques and results in a wide range of useful applications including: 1) devices with nonlinear characteristics which may be considered as linear over certain subregions; 2) networks whose response to changes in applied signal frequency or magnitude may be approximated by piecewise-linear asymptotes; 3) systems processing two or more signals simultaneously with different transfer or immitance characteristics for each signal; 4) circuits approximated by different equivalent circuits depending on the numerical values of critical parameters. Representative examples will illustrate these and similar applications. Procedures are presented to provide a logical, orderly, and effective approach to construct a model, to determine figures of merit, and to optimize the model for a prescribed region of operation or for a desired range of parameters. 相似文献