全文获取类型
收费全文 | 6797篇 |
免费 | 29篇 |
国内免费 | 16篇 |
专业分类
航空 | 3228篇 |
航天技术 | 2420篇 |
综合类 | 20篇 |
航天 | 1174篇 |
出版年
2021年 | 60篇 |
2019年 | 43篇 |
2018年 | 142篇 |
2017年 | 98篇 |
2016年 | 98篇 |
2015年 | 57篇 |
2014年 | 173篇 |
2013年 | 191篇 |
2012年 | 199篇 |
2011年 | 257篇 |
2010年 | 181篇 |
2009年 | 310篇 |
2008年 | 380篇 |
2007年 | 193篇 |
2006年 | 157篇 |
2005年 | 194篇 |
2004年 | 165篇 |
2003年 | 221篇 |
2002年 | 144篇 |
2001年 | 230篇 |
2000年 | 120篇 |
1999年 | 151篇 |
1998年 | 176篇 |
1997年 | 129篇 |
1996年 | 153篇 |
1995年 | 202篇 |
1994年 | 210篇 |
1993年 | 103篇 |
1992年 | 148篇 |
1991年 | 80篇 |
1990年 | 62篇 |
1989年 | 150篇 |
1988年 | 66篇 |
1987年 | 65篇 |
1986年 | 70篇 |
1985年 | 163篇 |
1984年 | 166篇 |
1983年 | 129篇 |
1982年 | 143篇 |
1981年 | 192篇 |
1980年 | 58篇 |
1979年 | 58篇 |
1978年 | 56篇 |
1977年 | 47篇 |
1976年 | 40篇 |
1975年 | 48篇 |
1974年 | 43篇 |
1973年 | 42篇 |
1972年 | 41篇 |
1969年 | 37篇 |
排序方式: 共有6842条查询结果,搜索用时 15 毫秒
991.
Nussinov MD Lysenko SV Kozlovskii MYu Pogodin YuS 《Journal of the British Interplanetary Society》1992,45(1):13-14
The use of charge-coupled devices is suggested as a means for detecting growth of micro-organism colonies. The accuracy of the method is determined by channel width and the sensitivity by the signal/noise ratio. The method was tested on a dense nutrient medium, which is to be considered more suitable to micro-organisms of the dry Martian soil than the water solution of nutrients employed in the Viking's strategy. 相似文献
992.
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
993.
994.
An investigation of the effects of drying and drying-rewetting cycles under vacuum conditions of 10(-2) torr at -30 degrees C on conidia of the atmospheric strain Penicillium chrysogenum from 48-77 km heights, collected by meteorological rockets found that survival and restoration of the initial physiological properties were possible through some very efficient protective cellular mechanisms. Such adaptive possibilities explain the widespread diffusion of microbial cells throughout the biosphere of our planet. 相似文献
995.
McCormick W.S. Tsui J.B.Y. Bakkie V.L. 《IEEE transactions on aerospace and electronic systems》1989,25(5):729-732
The instantaneous frequency measurement (IFM) receiver is capable of measuring the center frequency of single frequency pulses over a wide range (bandwidth) of center frequencies. Because of various constraints, the frequency resolution requirement results in long correlator delay times that reduce the single correlator bandwidth. A large bandwidth can be achieved only if two or more correlators are used. The problem of estimating frequency is then reduced to the simultaneous congruence problem of number theory. A design procedure is presented for solving the congruence problem for a given amount of noise protection, a stated frequency resolution, a minimum bandwidth, and a fixed level of precision (bits) in the IFM receiver 相似文献
996.
B. Kirov K. Georgieva D. Batchvarov A. Boneva R. Krasteva G. Stainov S. Klimov T. Dachev 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
The main purposes of experiment “Obstanovka” (“Environment” in Russian) consisting of several instruments are to measure a set of electromagnetic and plasma phenomena characterizing the space weather conditions, and to evaluate how such a big and highly energy consuming body as the International Space Station disturbs the surrounding plasma, and how the station itself is charged due to the operation of so many instruments, solar batteries, life supporting devices, etc. Two identical Langmuir electrostatic probes are included in the experiment “Obstanovka”. In this paper the Langmuir probes for “Obstanovka” experiment are described, including the choice of geometry (spherical or cylindrical), a more reliable method for the sweep voltage generation, an adaptive algorithm for the probe’s operation. Special attention is paid to the possibility for remote upgrading of the instrument from the ground using the standard communication channels. 相似文献
997.
Cosmic Research - We have considered procedure and results of the experimental study for spectral characteristics of self emission from laboratory models of electric thrusters with closed electron... 相似文献
998.
This work treats the question of large angle rotational maneuver and stabilization of an elastic spacecraft (spacecraft-beam-tip body configuration). It is assumed that the parameters of the system are completely unknown. An adaptive control law is derived for the rotational maneuver of the spacecraft. Using the adaptive controller, asymptotically decoupled control of the pitch angle of the space vehicle is accomplished, however this maneuver causes elastic deformation of the beam connecting the orbiter and tip body. For the stabilization of the zero dynamics (flexible dynamics), a stabilizer is designed using elastic mode velocity feedback. In the closed-loop system including the adaptive controller and the stabilizer, reference pitch angle trajectory tracking and vibration suppression are accomplished. Simulation results are presented to show the maneuver capability of the control system 相似文献
999.
It is generally accepted that the energy that drives coronal mass ejections (CMEs) is magnetic in origin. Sheared and twisted
coronal fields can store free magnetic energy which ultimately is released in the CME. We explore the possibility of the specific
magnetic configuration of a magnetic flux rope of field lines that twist about an axial field line. The flux rope model predicts
coronal observables, including heating along forward or inverse S-shaped, or sigmoid, topological surfaces. Therefore, studying
the observed evolution of such sigmoids prior to, during, and after the CME gives us crucial insight into the physics of coronal
storage and release of magnetic energy. In particular, we consider (1) soft-X-ray sigmoids, both transient and persistent;
(2) The formation of a current sheet and cusp-shaped post-flare loops below the CME; (3) Reappearance of sigmoids after CMEs;
(4) Partially erupting filaments; (5) Magnetic cloud observations of filament material. 相似文献
1000.
J Z Kiss R E Edelmann 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1999,24(6):755-762
In order to help resolve some of the controversy associated with ground-based research that has supported the starch-statolith theory of gravity perception in plants, we performed spaceflight experiments with Arabidopsis in Biorack during the January 1997 and May 1997 missions of the Space Shuttle. Seedlings of wild-type (WT) Arabidopsis, two reduced-starch strains, and a starchless mutant were grown in microgravity and then were given either a 30, 60, or 90 minute gravity stimulus on a centrifuge. By the 90 min 1-g stimulus, the WT exhibited the greatest magnitude of curvature and the starchless mutant exhibited the smallest curvature while the two reduced starch mutants had an intermediate magnitude of curvature. In addition, space-grown plants had two structural features that distinguished them from the controls: a greater number of root hairs and an anomalous hypocotyl hook structure. However, the morphological changes observed in the flight seedlings are likely to be due to the effects of ethylene present in the spacecraft. (Additional ground-based studies demonstrated that this level of ethylene did not significantly affect gravitropism nor did it affect the relative gravitropic sensitivity among the four strains.) Nevertheless, this experiment on gravitropism was performed the \"right way\" in that brief gravitational stimuli were provided, and the seedlings were allowed to express the response without further gravity stimuli. Our spaceflight results support previous ground-based studies of these and other mutants since increasing amounts of starch correlated positively with increasing sensitivity to gravity. 相似文献