全文获取类型
收费全文 | 3516篇 |
免费 | 683篇 |
国内免费 | 532篇 |
专业分类
航空 | 2119篇 |
航天技术 | 844篇 |
综合类 | 471篇 |
航天 | 1297篇 |
出版年
2024年 | 13篇 |
2023年 | 41篇 |
2022年 | 109篇 |
2021年 | 155篇 |
2020年 | 144篇 |
2019年 | 111篇 |
2018年 | 128篇 |
2017年 | 139篇 |
2016年 | 134篇 |
2015年 | 170篇 |
2014年 | 204篇 |
2013年 | 198篇 |
2012年 | 222篇 |
2011年 | 239篇 |
2010年 | 296篇 |
2009年 | 303篇 |
2008年 | 215篇 |
2007年 | 205篇 |
2006年 | 171篇 |
2005年 | 160篇 |
2004年 | 99篇 |
2003年 | 122篇 |
2002年 | 167篇 |
2001年 | 114篇 |
2000年 | 114篇 |
1999年 | 110篇 |
1998年 | 75篇 |
1997年 | 86篇 |
1996年 | 69篇 |
1995年 | 75篇 |
1994年 | 55篇 |
1993年 | 39篇 |
1992年 | 51篇 |
1991年 | 41篇 |
1990年 | 30篇 |
1989年 | 20篇 |
1988年 | 19篇 |
1987年 | 9篇 |
1986年 | 10篇 |
1985年 | 15篇 |
1984年 | 7篇 |
1983年 | 3篇 |
1982年 | 9篇 |
1981年 | 19篇 |
1980年 | 2篇 |
1979年 | 2篇 |
1978年 | 3篇 |
1976年 | 2篇 |
1974年 | 3篇 |
1965年 | 1篇 |
排序方式: 共有4731条查询结果,搜索用时 15 毫秒
941.
文章概括介绍了"发现号"宇宙飞船的布局结构。然后详细介绍了飞船用于火星探测的两种着陆舱的具体设计方案以及载人火星探测的任务剖面。最后分析了"发现号"宇宙飞船火星探测方案的关键可行技术和诸多设计优点。 相似文献
942.
943.
为提高发动机试车控制软件的可靠性,通过需求分析、概要设计、详细设计、软件测试等步骤实现了软件开发工程化。结合试验控制软件研制和使用特点,对软件质量管理的具体步骤,即从设计评审、测试、验证、文档及技术状态管理等方面对软件开发过程进行监督与管理,实现了软件开发的质量控制,达到了软件设计的透明性、继承性及高可靠性。 相似文献
944.
945.
由壳聚糖与环氧丙烷制备了羟丙基壳聚糖(HCS)。将其配制成水溶液,利用离子凝胶法,与多聚磷酸钠(TPP)反应,制备了粒径在0.6μm羟丙基壳聚糖微球。再用滴定水解法制备了四氧化三铁微粒,激光粒度分析显示滴定水解法制备的Fe3O4粒径分布较窄,粒径小。在此基础上采用交联聚合法制备了Fe3O4/HCS复合微球,微球为实心,四氧化三铁微粒被包裹于微球内部,形状规则,粒径约为0.8μm,经过磁响应分析表明Fe3O4/HCS复合微球具有磁响应性。 相似文献
946.
Energetic solar proton events within the energy interval 1–48 MeV at the stage of their decay are considered over the period of 1974–2001. The dependence of the characteristic decay time on the proton energy in the assumed power-law representation τ(E) =E ?n is analyzed for the events with an exponential decay form. The dependence of n on the heliolongitude of the flare (the particles source on the Sun) is studied. 相似文献
947.
Yu. P. Ulybyshev 《Cosmic Research》2008,46(2):133-145
Approximate numerical methods of optimization of spacecraft rendezvous trajectories are presented that make use of interior point algorithms for problems of linear programming of high dimensionality (tens to hundreds of thousands of variables). The basis of the methods is discretization of a trajectory into small segments in which maneuvers are allowed to be executed; for all segments sets of pseudo-impulses are introduced that determine the possible directions of the spacecraft thrust vector. The terminal conditions are presented in the form of a linear matrix equation. A matrix inequality for the sums of characteristic velocities of pseudo-impulses on each segment is used to make a transformation to the linear programming form. Spacecraft rendezvous trajectories are considered in the neighborhood of circular orbits with the use of multi-mode propulsion systems (including those with low thrust) and existence of boundary conditions at interior points and constraints on the time of operation of the propulsion system at separate segments of the trajectory. 相似文献
948.
The main goal of this paper is to get physically informative comprehensive data about dynamics of the solar magnetic field, geomagnetic field, and interplanetary magnetic field over large time scales. The total sunspot magnetic flux, aa and IDV indices of geomagnetic activity, the IMF strength, the dipole-octopole index of the large-scale magnetic field of the Sun, and the open magnetic flux are reconstructed for 400 years. The reconstruction of the π index of the large-scale polar magnetic field of the Sun is performed for 150 years. 相似文献
949.
The effect of Alfven-type oscillations in a coronal magnetic arch on modulation of the gyrosynchrotron radiation and development of the ballooning instability in the arch is considered. On the basis of the energy method and the method of normal modes, the expressions are obtained for increments of ballooning instability at its swinging by natural oscillations of the arch. The conclusion is drawn that bending oscillations, which do not actually compress the plasma and, therefore, represent the Alfven-type modes, unlike the radial oscillations, are capable, under solar corona conditions, to effectively swing ballooning instability and, as a consequence, play a part of a trigger for solar flares. The ballooning instability of coronal arches is shown to be capable of causing formation of helmet-shaped structures in the lower solar corona. On the basis of calculations of the intensity modulation depth and the degree of circular polarization of non-thermal gyrosynchrotron radiation, under the assumption of excited Alfven oscillations of a coronal arch, the conclusion is drawn, that microwave observations at a frequency of > 10 GHz can be used for studying the conditions of excitation and propagation of Alfven modes in flare loops. The consequences of obtained results are discussed using the flare on April 15, 2002 as an example. 相似文献
950.
The low-frequency component is investigated in the data of measurements performed onboard the Foton M-2 satellite with the three-component accelerometer TAS-3. Investigations consisted in comparison of this component with its calculated analog found from a reconstruction of the satellite’s attitude motion. The influence of the Earth’s magnetic field on the accelerometer readings is discovered by way of spectral analysis of the functions representing the results of determining the low-frequency microacceleration by two methods. After making correction for this influence, the results obtained by these two methods coincided within a root-mean-square error of less than 10?6 m/s2. 相似文献