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311.
The basic principles of selecting some design parameters of a lightweight airplane for the contemporary Russian market are presented. Recommendations for selecting these parameters with the service requirements specified are given based on the study performed. 相似文献
312.
313.
The Monitor-E spacecraft executed uncontrolled flight due to emergency situation, no telemetry information on parameters of the spacecraft’s
attitude motion being available. So, the problem arose to determine the spacecraft’s rotational motion from the accessible
indirect information—the electric current provided by solar batteries. In this paper the integrated statistical technique
is described, that allows one to solve this problem. The values of current, obtained over the time interval some tens of minutes
long, have been processed simultaneously by the least squares method using the integration of the equations of spacecraft’s
rotational motion. As a result of processing, the initial conditions of motion were estimated, and the spacecraft’s moments
of inertia were updated, as well as the angles, specifying solar batteries position in the spacecraft-fixed coordinate system.
The results of processing of 12 data sets are presented, which allowed us to reconstruct the actual rotational motion of the
spacecraft. 相似文献
314.
J.L. Hall D. Fairbrother T. Frederickson V.V. Kerzhanovich M. Said C. Sandy J. Ware C. Willey A.H. Yavrouian 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
This paper describes the design, fabrication and testing of a full scale prototype balloon intended for long duration flight in the upper atmosphere of Venus. The balloon is 5.5 m in diameter and is designed to carry a 45 kg payload at an altitude of 55 km. The balloon material is a 180 g/m2 multi-component laminate comprised of the following layers bonded together from outside to inside: aluminized Teflon film, aluminized Mylar film, Vectran fabric and a polyurethane coating. This construction provides the required balloon functional characteristics of low gas permeability, sulfuric acid resistance and high strength for superpressure operation. The design burst superpressure is 39,200 Pa which is predicted to be 3.3 times the worst case value expected during flight at the highest solar irradiance in the mission profile. The prototype is constructed from 16 gores with bi-taped seams employing a sulfuric acid resistant adhesive on the outside. Material coupon tests were performed to evaluate the optical and mechanical characteristics of the laminate. These were followed by full prototype tests for inflation, leakage and sulfuric acid tolerance. The results confirmed the suitability of this balloon design for use at Venus in a long duration mission. The various data are presented and the implications for mission design and operation are discussed. 相似文献
315.
S. I. Solovyev V. A. Mullayarov D. G. Baishev E. S. Barkova S. N. Samsonov 《Cosmic Research》2004,42(6):607-613
Modulation of the VLF emission and riometric absorption by Pc5 geomagnetic pulsations is studied in the period of strong geomagnetic disturbances on October 30–31, 2003. Some conclusions about the regime of pitch-angular diffusion into the loss cone are made. The better coincidence of VLF emission modulation with geomagnetic pulsations in other longitude sectors is explained by the global character of excitation of the pulsations and by damping of their amplitudes at the meridian of observation of the VLF emission, which is associated with intensification of auroral electrojets.Translated from Kosmicheskie Issledovaniya, Vol. 42, No. 6, 2004, pp. 632–639.Original Russian Text Copyright © 2004 by Solovyev, Mullayarov, Baishev, Barkova, Samsonov. 相似文献
316.
Spatial structure of the magnetosheath of the Earth was studied under the conditions when no sharp (more than 40° during 5
min) changes in the interplanetary magnetic field direction were observed. On the basis of 24 flights of the Interball-1 satellite through the magnetosheath, it is found that three regions differing from each other by parameters of the field
and plasma can be observed in the magnetosheath under the above-indicated conditions. These regions also differ from the solar
wind region before front of the Earth’s magnetospheric bow shock. Empirical distributions of parameters were studied in each
region. Taking into account the influence of the interplanetary magnetic field direction on the processes in the magnetosheath,
the cases of quasi-perpendicular and quasi-parallel shock waves were considered separately. The study showed that the distribution
of parameters in the selected regions (in the solar wind before front of the bow shock, in the magnetosheath behind the bow
shock (post-shock), in the region of the magnetosheath with minimal fluctuations in the field, and in the inner magnetosheath)
differ from each other at any interplanetary magnetic field direction. 相似文献
317.
A. N. Denisov N. V. Kuznetsov R. A. Nymmik M. I. Panasyuk N. M. Sobolevskii 《Cosmic Research》2010,48(6):509-516
In connection with projects of manned bases on the Moon it becomes topical to estimate radiation danger for their inhabitants.
In this paper we describe a method of evaluation of the radiation environment on the lunar surface produced by galactic and
solar cosmic rays. The roles of both primary and secondary radiations generated in the depth of the lunar soil under the action
of high-energy protons and nuclei are taken into account. Calculated fluxes of particles are used in order to estimate annual
averaged absorbed and equivalent local dose rates in tissues. It is established that in the lunar rock the contribution of
secondary neutrons to the dose rate exceeds that of protons. The contribution of the secondary particles generated by nuclei
of galactic cosmic rays to the dose rate is estimated. 相似文献
318.
V. Génot C. Jacquey M. Bouchemit M. Gangloff A. Fedorov B. Lavraud N. André L. Broussillou C. Harvey E. Pallier E. Penou E. Budnik R. Hitier B. Cecconi F. Dériot D. Heulet J.-L. Pinçon 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
AMDA (Automated Multi-Dataset Analysis), a new data analysis service, recently opened at the French Plasma Physics Data Center (CDPP). AMDA is developed according to the Virtual Observatory paradigm: it is a web-based facility for on-line analyses of space physics. Data may come from its own local database as well as remote ones. This tool allows the user to perform classical manipulations such as data visualization, parameter computation and data extraction. AMDA also offers innovative functionalities such as event searches on the content of the data in either visual or automated ways, generation, use and management of time tables (event lists). The general functionalities of AMDA are presented in the context of Space Weather with example scientific use cases. 相似文献
319.
V. G. Gainutdinov 《Russian Aeronautics (Iz VUZ)》2010,53(3):277-282
An algorithm is proposed for computer-aided calculation of required values of aircraft controlling moments and aerodynamic
moment coefficients for stable fulfillment of flight trajectories specified by design flight performance. 相似文献
320.
A three-dimensional design model of a helicopter tubular skid landing gear based on the application of the large beam displacement
theory is presented. The design model takes into account special features of constructive, physical and geometrical deformation
nonlinearity. The analysis of a real helicopter structure is given that confirms sufficient validity of calculation results
obtained using the model developed by comparing with the results of the finite element analysis. 相似文献