全文获取类型
收费全文 | 198篇 |
免费 | 29篇 |
国内免费 | 15篇 |
专业分类
航空 | 88篇 |
航天技术 | 89篇 |
综合类 | 11篇 |
航天 | 54篇 |
出版年
2024年 | 1篇 |
2023年 | 6篇 |
2022年 | 4篇 |
2021年 | 7篇 |
2020年 | 6篇 |
2019年 | 5篇 |
2018年 | 6篇 |
2017年 | 8篇 |
2016年 | 5篇 |
2015年 | 7篇 |
2014年 | 12篇 |
2013年 | 15篇 |
2012年 | 21篇 |
2011年 | 15篇 |
2010年 | 12篇 |
2009年 | 15篇 |
2008年 | 17篇 |
2007年 | 9篇 |
2006年 | 9篇 |
2005年 | 10篇 |
2004年 | 3篇 |
2003年 | 4篇 |
2002年 | 4篇 |
2001年 | 4篇 |
2000年 | 3篇 |
1999年 | 12篇 |
1998年 | 1篇 |
1997年 | 2篇 |
1996年 | 1篇 |
1995年 | 2篇 |
1994年 | 11篇 |
1993年 | 2篇 |
1992年 | 1篇 |
1991年 | 1篇 |
1989年 | 1篇 |
排序方式: 共有242条查询结果,搜索用时 15 毫秒
111.
L. Strachan Y-K. Ko A. V. Panasyuk D. Dobrzycka J. L. Kohl M. Romoli G. Noci S. E. Gibson D. A. Biesecker 《Space Science Reviews》1999,87(1-2):311-314
We constrain coronal outflow velocity solutions, resolved along the line-of-sight, by using Doppler dimming models of H I Lyman alpha and O VI 1032/1037 Å emissivities obtained with data from the Ultraviolet Coronagraph Spectrometer (UVCS) on SOHO. The local emissivities, from heliocentric heights of 1.5 to 3.0 solar radii, were determined from 3-D reconstructions of line-of-sight intensities obtained during the first Whole Sun Month Campaign (10 August to 8 September 1996). The models use electron densities derived from polarized brightness measurements made with the visible light coronagraphs on UVCS and LASCO, supplemented with data from Mark III at NCAR/MLSO. Electron temperature profiles are derived from 'freezing-in' temperatures obtained from an analysis of charge state data from SWICS/Ulysses. The work concentrates on neutral hydrogen outflow velocities which depend on modeling the absolute coronal H I Lyα emissivities. We use an iterative method to determine the neutral hydrogen outflow velocity with consistent values for the electron temperatures derived from a freezing-in model. 相似文献
112.
We present a preliminary analysis of two quiet Sun transition region areas observed with the SOHO/SUMER spectrometer, using
lines from oxygen, nitrogen and silicon. The average quiet Sun physical parameters are studied as a function of line intensity.
Systematic variations of line position and width with increasing intensity are found. A large number of small-scale active
points have been observed, and preliminary analysis of the physical properties and dynamics of these active features is presented.
A jet-like structure, found in an active point, is also investigated and its velocity along the line of sight determined.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
113.
David N. Burrows J. E. Hill J. A. Nousek J. A. Kennea A. Wells J. P. Osborne A. F. Abbey A. Beardmore K. Mukerjee A. D. T. Short G. Chincarini S. Campana O. Citterio A. Moretti C. Pagani G. Tagliaferri P. Giommi M. Capalbi F. Tamburelli L. Angelini G. Cusumano H. W. Bräuninger W. Burkert G. D. Hartner 《Space Science Reviews》2005,120(3-4):165-195
he Swift Gamma-Ray Explorer is designed to make prompt multiwavelength observations of gamma-ray bursts (GRBs) and GRB afterglows.
The X-ray telescope (XRT) enables Swift to determine GRB positions with a few arcseconds accuracy within 100 s of the burst onset.
The XRT utilizes a mirror set built for JET-X and an XMM-Newton/EPIC MOS CCD detector to provide a sensitive broad-band (0.2–10 keV) X-ray imager with effective area of > 120 cm2 at 1.5 keV, field of view of 23.6 × 23.6 arcminutes, and angular resolution of 18 arcseconds (HPD). The detection sensitivity
is 2×10−14 erg cm−2 s−1 in 104 s. The instrument is designed to provide automated source detection and position reporting within 5 s of target acquisition.
It can also measure the redshifts of GRBs with Fe line emission or other spectral features. The XRT operates in an auto-exposure
mode, adjusting the CCD readout mode automatically to optimize the science return for each frame as the source intensity fades.
The XRT will measure spectra and lightcurves of the GRB afterglow beginning about a minute after the burst and will follow
each burst for days or weeks.
Dedicated to David J. Watson, in memory of his valuable contributions to this instrument. 相似文献
114.
叙述了美国MTS公司生产的MTS-810(809)系列电液伺服疲劳试验机负荷系统、DC检测器和量程校准模块的原理、调整方法和力值校准方法。 相似文献
115.
116.
Bagrat Mailyan Ashot Chilingarian 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
A study of daily variations of secondary Cosmic Rays (CR) is performed using data on charged and neutral CR fluxes. Particle detectors of Aragats Space-Environmental Center (ASEC), Space Environmental Viewing and Analysis Network (SEVAN) and neutron monitors of the Neutron Monitor Database (NMDB) are used. ASEC detectors continuously register various species of secondary CR with different threshold energies and incident angles. NMDB joins data of 12 Eurasian neutron monitors. Data at the beginning of the 24th solar activity cycle are used to avoid biases due to solar transient events and to establish a benchmark for the monitoring of solar activity in the new started solar cycle. 相似文献
117.
研究了环氧乙烯基酯树脂基体及其复合材料的耐环境老化性能,包括耐湿热性能、耐自然老化性能及耐紫外光老化性能。研究结果表明,环氧乙烯基酯树脂体系具有良好的力学性能、耐湿热性能,在环境老化及耐紫外光辐射老化试验中表现出一定的稳定性,且工艺操作简便,可以作为户外基础设施用复合材料。 相似文献
118.
载人航天器舱门快速检漏仪是载人航天器舱门及其对接机构对接面气密性检测的测试仪器。为了验证舱门快速检漏仪的可靠性指标水平,按照寿命型和计量型可靠性试验方法的基本思路,通过分析其功能、工作原理和主要故障模式,确定了可靠性特征量,提出了舱门快速检漏仪的可靠性验证试验方法,包括试验方法的选择、试验件状态、试验条件的确定、试验程序、故障判据及可靠性评估方法,并给出了评估结果。 相似文献
119.
考虑月球扁率修正的月球卫星自主导航 总被引:1,自引:0,他引:1
针对月球扁率对月球紫外敏感器的月心方向矢量确定的不利影响,研究了月球紫外敏感器的测量原理和敏感到月平边缘时满足的几何约束,提出了一种考虑月球扁率的月心矢量确定方法。并进一步的结合地球敏感器和太阳敏感器的测量信息,研究了基于日地月方位信息的月球卫星自主轨道算法,并评估了月球方位确定算法对导航精度的影响。仿真结果表明,在太阳敏感器、地球敏感器和月球敏感器的精度分别为0.02°(3σ)、 0.05°(3σ) 和0.1°(3σ)的假设下,考虑月球扁率修正的月球卫星的自主导航位置精度能达到300m(3σ),导航速度误差能达到0.6m/s(3σ), 从而保证了环月卫星的导航精度。 相似文献
120.
电离层综合探测器数据采集处理单元设计研究 总被引:1,自引:0,他引:1
电离层综合探测器(CDI)是一种面向快速响应航天器平台、用于原位综合探测电离层等离子体及未完全电离中性气体的新概念空间环境探测仪器, 实现了对常规平板朗缪尔探针、阻滞势分析器和离子阱质量分析器的小型化、一体化设计与集成. 本文基于USB2.0接口和FPGA (Field-Programmable Gate Array)技术, 选用高集成度的COTS (Commercial-Off-The-Shelf)器件, 对CDI多通道数据采集处理单元的系统方案和硬件设计进行研究, 并对FPGA的逻辑资源利用情况和Fusion器件内部ADC采样以及FIFO (First Input First Output)读写时序进行了仿真和分析. 相似文献