全文获取类型
收费全文 | 3892篇 |
免费 | 8篇 |
国内免费 | 8篇 |
专业分类
航空 | 1762篇 |
航天技术 | 1429篇 |
综合类 | 10篇 |
航天 | 707篇 |
出版年
2021年 | 30篇 |
2018年 | 62篇 |
2017年 | 54篇 |
2016年 | 48篇 |
2015年 | 26篇 |
2014年 | 65篇 |
2013年 | 109篇 |
2012年 | 91篇 |
2011年 | 155篇 |
2010年 | 108篇 |
2009年 | 152篇 |
2008年 | 198篇 |
2007年 | 112篇 |
2006年 | 81篇 |
2005年 | 112篇 |
2004年 | 128篇 |
2003年 | 124篇 |
2002年 | 81篇 |
2001年 | 120篇 |
2000年 | 63篇 |
1999年 | 91篇 |
1998年 | 109篇 |
1997年 | 78篇 |
1996年 | 70篇 |
1995年 | 114篇 |
1994年 | 125篇 |
1993年 | 64篇 |
1992年 | 76篇 |
1991年 | 33篇 |
1990年 | 42篇 |
1989年 | 69篇 |
1988年 | 31篇 |
1987年 | 28篇 |
1986年 | 38篇 |
1985年 | 128篇 |
1984年 | 114篇 |
1983年 | 95篇 |
1982年 | 84篇 |
1981年 | 157篇 |
1980年 | 32篇 |
1979年 | 34篇 |
1978年 | 38篇 |
1977年 | 34篇 |
1976年 | 29篇 |
1975年 | 34篇 |
1974年 | 30篇 |
1973年 | 31篇 |
1972年 | 41篇 |
1971年 | 22篇 |
1970年 | 22篇 |
排序方式: 共有3908条查询结果,搜索用时 0 毫秒
991.
V. G. Zaitsev 《Russian Aeronautics (Iz VUZ)》2008,51(3):232-237
The vibroloading criteria are described to determine vibrations at the points of FV onboard equipment mounting. The generalized characteristics of vibroloading in the equipment tests are proposed and a method is considered that makes it possible to solve a problem of inconsistency between the three-dimensional loading in service and coordinate loading in tests. 相似文献
992.
V. G. Eselevich 《Space Science Reviews》1982,32(1-2):65-81
Results of laboratory experiments on the study of collisionless shock wave structure in plasmas with and without a magnetic field are summarized, and comparisons with theoretical inferences are made. Consideration is given to the clarification of the collisionless dissipation mechanism and to the causes that bring it about. Transition conditions from one type of shock wave to another are analyzed. The relationship between laboratory experiments and the Earth bow shock measurements is also examined.An invited paper presented at STIP Workshop on Shock Waves in the Solar Corona and Interplanetary Space, 15–19 June, 1980, Smolenice, Czechoslovakia. 相似文献
993.
D.R. Croley G.C. Spitale 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1998,21(12):1683-1687
Solar heavy ions from the JPL Solar Heavy Ion Model have been transported into low earth orbit using the Schulz cutoff criterion for L-shell access by ions of a specific charge to mass ratio. The NASA Brouwer orbit generator was used to get L values along the orbit at 60 second time intervals. Heavy ion fluences of ions 2≤Z≤92 have been determined for the LET range 1 to 130 MeV-cm2/mg by 60, 120 or 250 mils of aluminum over a period of 24 hours in a 425 km circular orbit inclined 51°. The ion fluence is time dependent in the sense that the position of the spacecraft in the orbit at the flare onset time fixes the relationship between particle flux and spacecraft passage through high L-values where particles have access to the spacecraft. 相似文献
994.
Lee F.C.Y. Wilson T.G. Feng S.Y.M. 《IEEE transactions on aerospace and electronic systems》1973,(4):571-584
A familiar two-transistor saturable-core parallel inverter is modeled as a nonlinear negative resistance in parallel with energy-storage elements. The techniques of singular-point analysis are combined with piecewise linear techniques to permit determination of solution trajectories on the phase plane. Clear insight is provided, not only into steady-state oscillation, but also into transient behavior of the circuit. Experimental results confirming the analytical model are included. 相似文献
995.
G.S. Lakhina S.V. SinghA.P. Kakad 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
A general model for the ion- and electron-acoustic solitons and double layers in a multi-component unmagnetized plasma consisting of background electrons, counter-streaming electron beams and ions is discussed. The model is based on the multi-fluid equations and the Poisson equation, and uses the Sagdeev pseudo-potential techniques. For identical counter-streaming electron beams and depending upon the plasma parameters, three types of solutions, namely, ion-acoustic, slow and fast electron-acoustic soliton/double layer, are possible. Generally, the ion acoustic solitons have positive potentials, slow-electron acoustic solitons have negative potentials and fast electron-acoustic solitons and double layers can have either positive or negative potentials depending on the core electron density. As beam speed is increased, first ion-acoustic and then slow electron-acoustic solitons disappear. At large beam speed, only fast electron-acoustic solitons/double layers survive. The results may be relevant to the observations of the electrostatic solitary waves (ESWs) observed in the Earth’s magnetosphere. 相似文献
996.
S.G. Wang J.K. Shi X. Wang G.J. Wang H.F. Zhang G.M. Chen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
This work is a continuation of the previous article and it focuses on low solar activity and modeling effort. NeQuick model uses Epstein layer formalism to model each part of the profile. We study the diurnal and seasonal variations of B2bot, ΔB2 (B2best − B2NeQuick2) and R (B2best/B2NeQuick 2) at Hainan station during low solar activity. The results show it is possible to improve the B2bot parameter of the NeQuick model at that region during low solar activity. Then, we use a function ?(t) with LT in different seasons to correct the B2bot formula of NeQuick 2. The correction shows that (1) By the correction formula, the B2bot of NeQuick is improved. The maximum standard deviation is improved for 9 km. (2) The correction formula is more effective in summer than in equinox and winter and performs better during early morning hours than during the rest of the day. 相似文献
997.
W. Hausleitner G. Kirchner S. Krauss J. Weingrill R. Pail H. Goiginger D. Rieser 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Satellite gravity field missions such as CHAMP, GRACE and GOCE are designed as low Earth orbiting spacecraft (LEO) with orbit heights of about 250–500 km. The challenging mission objectives require a very precise knowledge of the satellite orbit position in space. For these missions precise orbit information is typically provided by GPS satellite-to-satellite tracking (SST) observations supported by satellite laser ranging (SLR). 相似文献
998.
We have analyzed UV photospheric lines of seven O-type binaries, by means of crosscorrelation and Doppler tomographic methods, with the goal of estimating the physical properties of the individual stars. These systems are HD 1337 (AO Cas), HD 47129 (Plaskett's star), HD 57060 (29 UW CMa), HD 37043 (Iota Ori), HD 215835 (DH Cep), HD 152218, and HD 152248. Mass ratios have been obtained primarily from a cross-correlation technique, but also by several other techniques. The tomographic techniques allow us to separate the spectra of the components. We then can estimate the individual spectral types and luminosity classes of the stars (and henceT eff and logg, respectively), the luminosity ratio, and projected rotational velocities. We discuss the physical properties of these O-type binaries. These are some of the early results of a large scale project involving 36 O-type double-lined binary systems (from the catalog of Battenet al. 1989) which we will study using IUE and complementary ground-based data. 相似文献
999.
Krishnamurthy J. Pradeep G.L. 《IEEE transactions on aerospace and electronic systems》1977,(2):120-126
Effects of cochannel interference and synchronization error of the carrier phase on the probability of error in binary communications are considered. Several bounds on the probability of error are proposed. The bounds are easy to compute and do not require complete statistical characterization of the errors. They turn out to be simple linear combinations of error probabilities with no cochannel interferences and no phase errors. Several illustrative examples are given which show that the bounds can be tight. 相似文献
1000.