全文获取类型
收费全文 | 9113篇 |
免费 | 1993篇 |
国内免费 | 1699篇 |
专业分类
航空 | 6174篇 |
航天技术 | 2387篇 |
综合类 | 1217篇 |
航天 | 3027篇 |
出版年
2024年 | 55篇 |
2023年 | 134篇 |
2022年 | 319篇 |
2021年 | 408篇 |
2020年 | 389篇 |
2019年 | 282篇 |
2018年 | 327篇 |
2017年 | 370篇 |
2016年 | 324篇 |
2015年 | 449篇 |
2014年 | 547篇 |
2013年 | 569篇 |
2012年 | 650篇 |
2011年 | 673篇 |
2010年 | 760篇 |
2009年 | 687篇 |
2008年 | 593篇 |
2007年 | 531篇 |
2006年 | 458篇 |
2005年 | 392篇 |
2004年 | 283篇 |
2003年 | 284篇 |
2002年 | 312篇 |
2001年 | 272篇 |
2000年 | 304篇 |
1999年 | 320篇 |
1998年 | 320篇 |
1997年 | 255篇 |
1996年 | 240篇 |
1995年 | 214篇 |
1994年 | 203篇 |
1993年 | 160篇 |
1992年 | 144篇 |
1991年 | 130篇 |
1990年 | 95篇 |
1989年 | 87篇 |
1988年 | 79篇 |
1987年 | 50篇 |
1986年 | 31篇 |
1985年 | 24篇 |
1984年 | 17篇 |
1983年 | 10篇 |
1982年 | 12篇 |
1981年 | 21篇 |
1980年 | 2篇 |
1979年 | 3篇 |
1978年 | 3篇 |
1976年 | 2篇 |
1974年 | 3篇 |
1965年 | 5篇 |
排序方式: 共有10000条查询结果,搜索用时 15 毫秒
61.
本文运用应力—强度干涉理论,推导了应力为Ⅰ型极小值分布,强度为威布尔分布的可靠度计算公式,并对冗长的计算公式进行简化,在简化公式的基础上,运用一定的数学技巧,改变积分公式中的积分变量和上下限。将被积函数化成在某一区域内的可积函数。采用de Boor编制的一种严谨的自适应Romberg外推格式的FORTRAN程序进行数值积分。对应予不同的组合参数,给出应力服从Ⅰ型极小值分布,强度服从威布尔分布的可靠度数值。本文最后讨论了服从这两种分布的组合参数的变化对可算度数值变化的影响。 相似文献
62.
Yang Yi Shi Baochang He Yanyan 《遥测遥控》2007,(4)
基于自相关理想序列和正交矩阵建立一类统一的具有零(低)相关区的扩频序列构造方法,并对其相关特性进行分析和证明。该类方法可通过序列和矩阵的任意选取,统一地构造二元、三元、多相、复数的ZCZ(LCZ)序列集,且构造简单、形式统一,通用性更好,适用于准同步CDMA(QS-CDMA)系统。 相似文献
63.
This article studies the efficiency of ejecting waste generated by the life support system (LSS) of a manned spacecraft to reduce initial mass on low earth orbit. The spacecraft is used for a long-duration interplanetary mission and is equipped with either a chemical or a nuclear-thermal propulsion system. For this study we simulate an optimal control problem for a given spacecraft maneuver. An impulsive approximation of the optimal interplanetary spacecraft trajectory is assumed, which allows us to reduce the general optimal control problem to hierarchic structure of 'outer' and 'inner' subproblems. This structure is analyzed using the Pontryagin's Maximum principle. Numerical results, illustrating the efficiency of waste ejection are shown for typical Earth-Mars transfer trajectories. This results confirm in theory that using a waste ejection system makes an early manned Mars mission possible without having to design and build new, advanced biological LSS. 相似文献
64.
65.
In 1994–1995 Lavochkin Association (Russia) together with the other enterprises in accordance with technical requirements of the Russian Space agency, developed a new Russian communication satellite of a small class that will operate in both the geostationary (GSO) and high-elliptical (HEO) orbits. This satellite may be injected into operational orbits using a SOYUZ-2 launch vehicle (LV) and a FREGAT upper stage (US) from Plesetsk and Baykonur space launch sites (SLS).The main reason for creating such a satellite was to decrease the cost of the support and development of the Russian communication geostationary satellites group.Russian satellites Horizont, Express, Ekran and Gals, which operate in GSO, are the basis of the space segment for communications, radio and TV broadcasting. All of these satellites are injected into GSO by the PROTON LV. PROTON is a launch vehicle of a heavy class. The use of a middle class LV instead of a heavy class will allow to reduce considerably the launch cost. The change of a heavy class LV to a LV of middle class determined one economic reason for this project. Besides, the opportunity to launch S/C into GSO from Russian Plesetsk SLS increases the independence of Russia in the domain of space communications, despite the presence of the contract with Kazachstan about the rent of Baykonur SLS. Finally, use of small satellites with a rather small number of transponders is more effective than the use of big satellites. It will allow also to increase a satellite group (by the launch of additional satellites) precisely in accordance to the development of the ground segment. 相似文献
66.
较详细地对复合材料壳体与喷管卡环连接结构进行了有限元应力,应变分析,对卡环,接头及倒锥等多体接触问题进行研究;对“I”型及“L”型卡环结构分别进行了计算和比较,并给出计算结果及结果分析。 相似文献
67.
国外航天侦察相机和测绘相机发展概况 总被引:5,自引:0,他引:5
航天侦察和测绘是战略武装必不可少的组成部分,航天侦察和测绘相机是对地观测卫星的有效载荷。 该文将简要介绍国外航天侦察和测绘相机发展概况、水平和发展趋势。 相似文献
68.
In 1994-1995 Lavochkin Association (Russia) together with the other enterprises in accordance with technical requirements of the Russian Space agency, developed a new Russian communication satellite of a small class that will operate in both the geostationary (GSO) and high-elliptical (HEO) orbits. This satellite may be injected into operational orbits using a SOYUZ-2 launch vehicle (LV) and a FREGAT upper stage (US) from Plesetsk and Baykonur space launch sites (SLS).The main reason for creating such a satellite was to decrease the cost of the support and development of the Russian communication geostationary satellites group.Russian satellites Horizont, Express, Ekran and Gals, which operate in GSO, are the basis of the space segment for communications, radio and TV broadcasting. All of these satellites are injected into GSO by the PROTON LV. PROTON is a launch vehicle of a heavy class. The use of a middle class LV instead of a heavy class will allow to reduce considerably the launch cost. The change of a heavy class LV to a LV of middle class determined one economic reason for this project. Besides, the opportunity to launch S/C into GSO from Russian Plesetsk SLS increases the independence of Russia in the domain of space communications, despite the presence of the contract with Kazachstan about the rent of Baykonur SLS. Finally, use of small satellites with a rather small number of transponders is more effective than the use of big satellites. It will allow also to increase a satellite group (by the launch of additional satellites) precisely in accordance to the development of the ground segment. 相似文献
69.
70.