全文获取类型
收费全文 | 84337篇 |
免费 | 15841篇 |
国内免费 | 11325篇 |
专业分类
航空 | 62034篇 |
航天技术 | 18615篇 |
综合类 | 8013篇 |
航天 | 22841篇 |
出版年
2024年 | 263篇 |
2023年 | 1133篇 |
2022年 | 3045篇 |
2021年 | 3561篇 |
2020年 | 3419篇 |
2019年 | 2742篇 |
2018年 | 3321篇 |
2017年 | 3731篇 |
2016年 | 2755篇 |
2015年 | 3578篇 |
2014年 | 4574篇 |
2013年 | 4809篇 |
2012年 | 5483篇 |
2011年 | 6215篇 |
2010年 | 6138篇 |
2009年 | 6467篇 |
2008年 | 6294篇 |
2007年 | 5629篇 |
2006年 | 5173篇 |
2005年 | 4234篇 |
2004年 | 3162篇 |
2003年 | 2582篇 |
2002年 | 2261篇 |
2001年 | 2428篇 |
2000年 | 2056篇 |
1999年 | 2068篇 |
1998年 | 1543篇 |
1997年 | 1133篇 |
1996年 | 1178篇 |
1995年 | 1262篇 |
1994年 | 1305篇 |
1993年 | 690篇 |
1992年 | 681篇 |
1991年 | 409篇 |
1990年 | 367篇 |
1989年 | 501篇 |
1988年 | 299篇 |
1987年 | 388篇 |
1986年 | 274篇 |
1985年 | 511篇 |
1984年 | 425篇 |
1983年 | 338篇 |
1982年 | 341篇 |
1981年 | 481篇 |
1980年 | 203篇 |
1979年 | 163篇 |
1978年 | 175篇 |
1975年 | 162篇 |
1974年 | 162篇 |
1972年 | 156篇 |
排序方式: 共有10000条查询结果,搜索用时 218 毫秒
981.
NEPE固体推进剂动态力学性能的研究 总被引:5,自引:0,他引:5
利用傅立叶红外光谱仪及扭辫法研究了不同粘合剂系统中异氰酯活性基团与羟基基团的当量比值,扩链剂以及预聚时间对NEPE固体推剂的次级转变温度、等参量的影响。研究结果对该类推进剂配设计和工艺参量选择提供了必要的实验依据。 相似文献
982.
983.
984.
The high inclination orbit for the International Space Station poses a risk to astronauts on EVA during occasional periods of enhanced high energy particle flux from the sun known as Solar Particle Events. We are currently unable to predict these events within the few-hour lead time required for evasive action. Compounding the threat is the fact that station construction occurs during increasing solar activity and through the peak of the solar cycle. In this paper we present an overview of the risk, the current methods to provide forecasts of SPEs, and potential risk mitigation options. 相似文献
985.
Extra-vehicular activity (EVA) has a significant role during extended space flights. It demonstrates that humans can survive and perform useful work outside the Orbital Space Stations (OSS) while wearing protective space suits (SS). When the International Space Station 'Alpha' (ISSA) is fully operational, EVA assembly, installation, maintenance and repair operations will become an everyday repetitive work activity in space. It needs new ergonomic evaluation of the work/rest schedule for an increasing of the labor amount per EVA hour. The metabolism assessment is a helpful method to control the productivity of the EVA astronaut and to optimize the work/rest regime. Three following methods were used in Russia to estimate real-time metabolic rates during EVA: 1. Oxygen consumption, computed from the pressure drop in a high pressure bottle per unit time (with actual thermodynamic oxygen properties under high pressure and oxygen leakage taken into account). 2. Carbon dioxide production, computed from CO2 concentration at the contaminant control cartridge and gas flow rate in the life support subsystem closed loop (nominal mode) or gas leakage in the SS open loop (emergency mode). 3. Heat removal, computed from the difference between the temperatures of coolant water or gas and its flow rate in a unit of time (with assumed humidity and wet oxygen state taken into account). Comparison of heat removal values with metabolic rates enables us to determine the thermal balance during an operative medical control of EVA at "Salyut-6", "Salyut-7" and "Mir" OSS. Complex analysis of metabolism, body temperature and heat rate supports a differential diagnosis between emotional and thermal components of stress during EVA. It gives a prognosis of human homeostasis during EVA. Available information has been acquired into an EVA data base which is an effective tool for ergonomical optimization. 相似文献
986.
A relatively general formulation for studying the dynamics and control of an arbitrary spacecraft with interconnected flexible bodies has been developed accounting for transient system properties, shift in the center of mass, shear deformations, rotary inertias and geometric nonlinearities. This self-contained, comprehensive, numerical algorithm using system modes is applicable to a large class of spacecraft configurations of contemporary and future interests. Here, versatility of the approach is demonstrated through the dynamics and control studies aimed at the evolving Space Station Freedom. 相似文献
987.
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
988.
Rhoda Shaller Hornstein Gerald L. Shinkle Jerry D. Weiler John K. Willoughby 《Acta Astronautica》1991,25(12):793-798
The widely distributed nature of the Space Station Freedom program, plus continuous multi-year operations will force program planners to develop innovative planning concepts. The traditional centralized planning operation will not be adequate. It will be replaced by multiple small planning centers working within guidelines issued by a central planning authority. Plans will not be optimized; rather, operating efficiency and user flexibility will be blended to satisfy program goals. The key to this new approach is the application of new planning methodologies and system development technologies to accommodate distributed resources that must be integrated. Resources will be distributed to the multiple planning entities in such a way that, when the several plans are built and then integrated, they will fit together with minimal modification. The plan itself will be an envelope schedule containing resource limits and constraint boundaries within which users will be free to make choices of the specific activities they will execute, up to the time of execution. Some level of margin within program guidelines will be built in to allow for variation and unforeseen change. This paper presents the authors' recommended planning approach and cites two NASA systems being developed that will utilize these resource distribution/integration planning concepts, methodologies and development technologies. 相似文献
989.
根据气动布局的基本原理,结合低RCS要求,设计了一种鸭式布局、带边条的翼身融合无人飞行器外形,实验结果表明,该外形不仅具有低RCS特征,而且具有良好的气动特性,升阻比达到8左右。 相似文献
990.