全文获取类型
收费全文 | 1439篇 |
免费 | 35篇 |
国内免费 | 32篇 |
专业分类
航空 | 660篇 |
航天技术 | 622篇 |
综合类 | 41篇 |
航天 | 183篇 |
出版年
2022年 | 12篇 |
2021年 | 17篇 |
2020年 | 13篇 |
2019年 | 14篇 |
2018年 | 14篇 |
2017年 | 11篇 |
2016年 | 19篇 |
2015年 | 8篇 |
2014年 | 40篇 |
2013年 | 49篇 |
2012年 | 43篇 |
2011年 | 58篇 |
2010年 | 43篇 |
2009年 | 73篇 |
2008年 | 122篇 |
2007年 | 39篇 |
2006年 | 41篇 |
2005年 | 64篇 |
2004年 | 42篇 |
2003年 | 37篇 |
2002年 | 35篇 |
2001年 | 58篇 |
2000年 | 25篇 |
1999年 | 38篇 |
1998年 | 45篇 |
1997年 | 18篇 |
1996年 | 38篇 |
1995年 | 31篇 |
1994年 | 40篇 |
1993年 | 25篇 |
1992年 | 39篇 |
1991年 | 14篇 |
1990年 | 15篇 |
1989年 | 39篇 |
1988年 | 17篇 |
1987年 | 12篇 |
1986年 | 16篇 |
1985年 | 27篇 |
1984年 | 39篇 |
1983年 | 31篇 |
1982年 | 29篇 |
1981年 | 37篇 |
1980年 | 8篇 |
1979年 | 9篇 |
1978年 | 7篇 |
1977年 | 8篇 |
1975年 | 6篇 |
1971年 | 6篇 |
1970年 | 5篇 |
1969年 | 6篇 |
排序方式: 共有1506条查询结果,搜索用时 15 毫秒
101.
102.
文章对星载设备遥测遥控电路中使用1553B总线技术进行了探讨,分析了星载设备采用1553B总线技术后的特点,提出了可行的实现途径。 相似文献
103.
104.
提高总增压比是下一代民用发动机的重要发展趋势之一,有必要对于这一特征的涡扇发动机进行循环参数的研究。利用已有基于Gasturb平台开发的0维变比热部件级性能计算模型,在发动机安装尺寸给定的前提下,总增压比由40提高至60,分析比较不同构型的直驱风扇方案与齿轮传动方案对部件效率,冷却水平对循环参数优选过程的影响。结果表明:为实现更低耗油率,采用更高设计循环增压比,需要部件效率平均提高1%,冷却水平提高20%,此时性能均优于现有的大涵道比涡扇发动机GTF-11。因此,若技术水平未能达到预期目标,则需匹配合适的增压比才能达到更低的耗油率。 相似文献
105.
Y. I. Yermolaev I. G. Lodkina N. S. Nikolaeva M. Y. Yermolaev M. O. Riazantseva 《Cosmic Research》2017,55(3):178-189
This paper discusses the errors in analyzing solar-terrestrial relationships, which result from either disregarding the types of interplanetary drivers in studying the magnetosphere response on their effect or from the incorrect identification of the type of these drivers. In particular, it has been shown that the absence of selection between the Sheath and ICME (the study of so-called CME-induced storms, i.e., magnetic storms generated by CME) leads to errors in the studies of interplanetary conditions of magnetic storm generation, because the statistical analysis has shown that, in the Sheath + ICME sequences, the largest number of storm onsets fell on the Sheath, and the largest number of storms maxima fell at the end of the Sheath and the beginning of the ICME. That is, the situation is observed most frequently when at least the larger part of the main phase of storm generation falls on the Sheath and, in reality, Sheath-induced storms are observed. In addition, we consider several cases in which magnetic storms were generated by corotating interaction regions, whereas the authors attribute them to CME. 相似文献
106.
为获得整体式固冲发动机转级过程中进气道堵盖(包括入口堵盖与出口堵盖)打开过程的流动形态,建立了进气道二维模型,利用Fluent动网格技术和UDF方法,开展了进气道堵盖打开过程非稳态流场研究。结果表明,在入口堵盖打开前,进气道前端形成强烈的弓形激波;在入口打开、出口未开的过程中,沿进气道轴向各监测点压强呈现周期性变化,振荡频率为100 Hz左右,出口堵盖位置压强振荡幅值为0.53 MPa;在出口打开后,补燃室残余热量形成的压强峰导致进气道在短时间内无法起动,随着背压降低至小于进气道再起动反压,进气道完全起动。 相似文献
107.
The Lunar Gravity Ranging System for the Gravity Recovery and Interior Laboratory (GRAIL) Mission 总被引:1,自引:0,他引:1
William M. Klipstein Bradford W. Arnold Daphna G. Enzer Alberto A. Ruiz Jeffrey Y. Tien Rabi T. Wang Charles E. Dunn 《Space Science Reviews》2013,178(1):57-76
The Lunar Gravity Ranging System (LGRS) flying on NASA’s Gravity Recovery and Interior Laboratory (GRAIL) mission measures fluctuations in the separation between the two GRAIL orbiters with sensitivity below 0.6 microns/Hz1/2. GRAIL adapts the mission design and instrumentation from the Gravity Recovery and Climate Experiment (GRACE) to a make a precise gravitational map of Earth’s Moon. Phase measurements of Ka-band carrier signals transmitted between spacecraft with line-of-sight separations between 50 km to 225 km provide the primary observable. Measurements of time offsets between the orbiters, frequency calibrations, and precise orbit determination provided by the Global Positioning System on GRACE are replaced by an S-band time-transfer cross link and Deep Space Network Doppler tracking of an X-band radioscience beacon and the spacecraft telecommunications link. Lack of an atmosphere at the Moon allows use of a single-frequency link and elimination of the accelerometer compared to the GRACE instrumentation. This paper describes the implementation, testing and performance of the instrument complement flown on the two GRAIL orbiters. 相似文献
108.
S. Yu. Mikheev I. I. Shkarban Y. A. Ryzhov S. A. Khartov M. M. Gorshkov R. P. Markov 《Russian Aeronautics (Iz VUZ)》2012,55(1):108-112
A process of manufacture of porous membranes made of aluminum foil (Al 99.99%) by the method of electrochemical anodic oxidation followed by a continuous barrier layer removal with ion-plasma irradiation is described. The membranes having a 8 mm diameter made from AL2O3 with a thickness from 2 to 5 microns thick with a regular channel arrangement are obtained. A possibility to change the channel diameter in the range of 20?C100 nm by adjusting voltage and temperature during the oxidation is shown. We present the experimental dependencies of aluminum and aluminum oxide sputtering coefficients on the energy and incidence angle of xenon ions within the energy range of 100??400 eV. 相似文献
109.
J. B. Blake P. A. Carranza S. G. Claudepierre J. H. Clemmons W. R. Crain Jr. Y. Dotan J. F. Fennell F. H. Fuentes R. M. Galvan J. S. George M. G. Henderson M. Lalic A. Y. Lin M. D. Looper D. J. Mabry J. E. Mazur B. McCarthy C. Q. Nguyen T. P. O’Brien M. A. Perez M. T. Redding J. L. Roeder D. J. Salvaggio G. A. Sorensen H. E. Spence S. Yi M. P. Zakrzewski 《Space Science Reviews》2013,179(1-4):383-421
This paper describes the Magnetic Electron Ion Spectrometer (MagEIS) instruments aboard the RBSP spacecraft from an instrumentation and engineering point of view. There are four magnetic spectrometers aboard each of the two spacecraft, one low-energy unit (20–240 keV), two medium-energy units (80–1200 keV), and a high-energy unit (800–4800 keV). The high unit also contains a proton telescope (55 keV–20 MeV). The magnetic spectrometers focus electrons within a selected energy pass band upon a focal plane of several silicon detectors where pulse-height analysis is used to determine if the energy of the incident electron is appropriate for the electron momentum selected by the magnet. Thus each event is a two-parameter analysis, an approach leading to a greatly reduced background. The physics of these instruments are described in detail followed by the engineering implementation. The data outputs are described, and examples of the calibration results and early flight data presented. 相似文献
110.
In a model experiment plants were grown in sealed chambers on expanded clay aggregate under the luminance of 150 W/m2 PAR and the temperature of 24 degrees C. Seven bacterial strains under investigation, replicated on nutrient medium surface in Petri dishes, were grown in the atmosphere of cultivated plants. Microbial response was evaluated by the difference between colony size in experiment and in control. In control, bacteria grew in the atmosphere of clean air. To study the effects of volatile metabolites of various plant on microbial growth, the experimental data were compared with the background values defined for each individual experiment. Expanded clay aggregate, luminance, temperature, and sealed chamber (without plants) for the background were the same. Volatile metabolites from 28-days old radish plants have been reliably established to have no effect on the growth of microbes under investigation. Metabolites of 30-days old dill and 50-days old garlic have been established to have reliable bacteriostatic effect on the growth of three bacterial strains. Dill and garlic have been found to have different range of effects of volatile substances on bacterial growth. Volatile metabolites of dill and garlic differed in their effect on the sensitivity spectrum of bacteria. An attempt has been made to describe the obtained data mathematically. 相似文献