全文获取类型
收费全文 | 229篇 |
免费 | 147篇 |
国内免费 | 29篇 |
专业分类
航空 | 253篇 |
航天技术 | 76篇 |
综合类 | 21篇 |
航天 | 55篇 |
出版年
2023年 | 11篇 |
2022年 | 13篇 |
2021年 | 14篇 |
2020年 | 18篇 |
2019年 | 10篇 |
2018年 | 9篇 |
2017年 | 6篇 |
2016年 | 7篇 |
2015年 | 6篇 |
2014年 | 12篇 |
2013年 | 15篇 |
2012年 | 19篇 |
2011年 | 17篇 |
2010年 | 18篇 |
2009年 | 14篇 |
2008年 | 19篇 |
2007年 | 13篇 |
2006年 | 12篇 |
2005年 | 13篇 |
2004年 | 7篇 |
2003年 | 8篇 |
2002年 | 3篇 |
2001年 | 8篇 |
2000年 | 14篇 |
1999年 | 14篇 |
1998年 | 10篇 |
1997年 | 18篇 |
1996年 | 10篇 |
1995年 | 13篇 |
1994年 | 10篇 |
1993年 | 6篇 |
1992年 | 8篇 |
1991年 | 3篇 |
1990年 | 6篇 |
1989年 | 10篇 |
1988年 | 2篇 |
1987年 | 8篇 |
1986年 | 1篇 |
排序方式: 共有405条查询结果,搜索用时 46 毫秒
141.
Gale Paulsen Kris Zacny Christopher B. Dreyer Attila Szucs Matt Szczesiak Chris Santoro Jack Craft Magnus Hedlund John Skok 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
We have developed a rock grinding and polishing mechanism for in situ planetary exploration based on abrasive disks, called Grinding Rocks Into Thin Sections (GRITS). Performance characteristics and design considerations of GRITS are presented. GRITS was developed as part of a broader effort to develop an in situ automated rock thin section (ISARTS) instrument. The objective of IS-ARTS was to develop an instrument capable of producing petrographic rock thin sections on a planetary science spacecraft. GRITS may also be useful to other planetary science missions with in situ instruments in which rock surface preparation are necessary. 相似文献
142.
是贤珠 《民用飞机设计与研究》2012,(1):61-65
由于反推力系统必须在模拟气动载荷下做试验,以验证反推力系统功能的安全可靠性。因此在液压系统地面模拟试验中需配置一套反推力装置加载系统,以实现对反推力在展开和收起过程中所受气动载荷的模拟。在简要介绍反推力系统及其加载系统的基础上,主要研究如何完成某型飞机反推力装置加载试验,并满足其性能要求。 相似文献
143.
144.
145.
为了研究一款液氧/甲烷发动机推力室多循环工作状态下的结构变形,拓展并验证了一种包括流动-传热分析和非线性有限元分析的热-结构分析方法。通过该方法得到了推力室热载荷与压力载荷分布,并分析了推力室在这些载荷下的应力应变响应。研究表明:推力室整体结构变形并非主要取决于热载荷,压力载荷引起的冷却通道底面弯曲在喷管扩张段尤其明显;后冷阶段产生的弹塑性拉伸应变大于热试阶段产生的压缩应变是导致每次循环结束后结构产生残余应变的直接原因;随着工作循环次数的增加,扩张段的冷却通道底角位置残余应变累积速率最快,该部位被确定为结构失效的潜在位置;增加冷却剂入口附近的通道底面厚度、减小后冷阶段与热试阶段的温差以及将冷却通道的尖锐底角设计为圆角可以成为抑制变形和减缓应变累积的备选措施。 相似文献
146.
考虑耦合效应的动量轮扰动测量 总被引:1,自引:0,他引:1
动量轮微振动是影响卫星姿态控制精度的重要因素.测量动量轮扰动的目的是掌握其扰动规律,进而采取相应的控制方法和隔离技术.由于动量轮的扰动频带很宽,扰动会与测试台的固有频率产生耦合.应用"动质量测试法"来定量地考察测试台刚度对扰动力测试的影响,并建立动量轮的力学模型,以得到不受影响的纯扰动.设计两种不同刚度的测试平台进行扰动测试.应用放大系数对测试结果进行修正,得到消除测试平台刚度影响的测试结果并进行比较.比较结果表明:动质量测试与理论建模结合法能够得到测试台的刚度对测试结果的影响. 相似文献
147.
F. Santoni F. Piergentili F. Graziani 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The nanosatellite UNICubeSAT is described, carrying a Broglio Drag Balance Instrument for neutral thermosphere density in situ measurements. The aim of the mission is to contribute to the development of accurate thermosphere models, achieving in situ, real time measurements of atmosphere density, that could be exploited for global atmosphere model validation and accurate short term (1–3 days) real time space weather forecasts. The satellite is inexpensive and swarms could be easily launched operating as a distributed sensor network to get simultaneous in situ local (not orbit averaged) measurements in multiple positions and orbit heights. The nanosatellite is based on the Cubesat standard architecture, weighing about 1 kg for 1-L volume. Atmospheric drag force is measured by the displacement of light plates exposed to the incoming particle flux seen by the spacecraft, applying the original three dimensional Broglio Drag Balance concept to a single nanosatellite axis. The instrument concept and its relation to the satellite bus is depicted, showing that many long term potential measurement error sources and biases can be removed in data processing if the spacecraft is spin stabilized. The expected accuracy in density measurements is 20%. The instrument cost is a fraction of that of accurate accelerometers. The onboard systems are based on commercial off the shelf components, in accordance with the short lifetime typical of aeronomy satellites. 相似文献
148.
149.
提出了一种多通道、高密度、高精度数据采集系统的设计方案.采用基于现场可编程逻辑门阵列(FPGA, Field Programmable Gate Arrays)内嵌软核的体系结构,实现了多通道数据的缓冲、格式转换、乒乓读写等流水操作,解决了多层CT(Computed Tomography)有限扫描时间内数据量大、时序要求严格和数据传输精确性要求高的问题;同时利用高精度电压源和精密电阻模拟了前端输入,设计了基于PXI(PCI eXtensions for Instrumentation)总线的虚拟仪器,精确测试了设计系统的性能且未额外引入噪声.方案已成功应用于多层CT中,同时也为数据采集提供一种借鉴. 相似文献
150.
Experiments in materials science on the ground and in reduced gravity using electrostatic levitators
Paul-Franois Paradis Takehiko Ishikawa Shinichi Yoda 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(12):2118-2125
To counter residual accelerations, dedicated levitators or positioners are necessary to support a host of materials science experiments on the ground and in microgravity. All levitators (e.g., aerodynamic, acoustic, electromagnetic, electrostatic, optical) have their own merits and limitations but the electrostatic scheme offers the combined advantages of processing millimeter-size objects, independent heating, quasi-spherical shape of molten materials, handling of materials under extreme temperatures for hours, virtually convection-free samples, and wide view around the samples for diagnostic. These attributes provide unique research opportunities in materials science on the ground as well as under reduced gravity. In particular, electrostatic levitators are very attractive to measure the physical and structural properties of equilibrium and non-equilibrium liquids, to synthesize multi-function materials, and to understand metastable phase formation, vitrification, and diffusion. In this paper, research and development carried out by the Japan Aerospace Exploration Agency over the years in the field of electrostatic levitation are summarized and the main results obtained in materials science are presented. 相似文献