全文获取类型
收费全文 | 82篇 |
免费 | 0篇 |
专业分类
航空 | 17篇 |
航天技术 | 13篇 |
综合类 | 6篇 |
航天 | 46篇 |
出版年
2018年 | 1篇 |
2017年 | 2篇 |
2015年 | 1篇 |
2014年 | 1篇 |
2013年 | 1篇 |
2011年 | 8篇 |
2010年 | 3篇 |
2009年 | 6篇 |
2008年 | 3篇 |
2007年 | 1篇 |
2006年 | 1篇 |
2005年 | 3篇 |
2004年 | 3篇 |
2003年 | 2篇 |
2002年 | 3篇 |
2001年 | 7篇 |
2000年 | 6篇 |
1999年 | 2篇 |
1997年 | 1篇 |
1996年 | 1篇 |
1995年 | 2篇 |
1994年 | 4篇 |
1993年 | 3篇 |
1992年 | 1篇 |
1991年 | 2篇 |
1990年 | 2篇 |
1989年 | 2篇 |
1988年 | 1篇 |
1985年 | 4篇 |
1982年 | 1篇 |
1967年 | 3篇 |
1966年 | 1篇 |
排序方式: 共有82条查询结果,搜索用时 125 毫秒
41.
This paper argues the need now to consider defining a vertical or spatial boundary between air space and outer space, which in turn effectively means defining the extent of air law and space law. Technology changes in aircraft, spacecraft, positioning systems and remote sensing, combined with the growth in the number of spacefaring nations, make the situation different from the early days of the space era when it was assumed that a boundary would be defined at a future indeterminate date. This article describes the background to the debates and the growing pressures of the questions of sovereignty concerning air and space law, and argues the case for a vertical or spatial boundary rather than a functional one. 相似文献
42.
43.
Philip R. Harris 《Space Policy》1989,5(4):273-278
A member of the Cal Space group convened to study ways of capitalizing on the past 20 years of investment in space, Philip R. Harris here outlines how he believes the US space effort can be galvanized to meet the challenges of the next decade. A new space ethos must be fostered within the national culture by broadening popular involvement in space enterprise. NASA should also be reformed to give it more independence and initiative. This calls for transformational leadership, committed to creating and communicating the vision of change. 相似文献
44.
Data policy is an important element of the initiative on Global Monitoring for Environment and Security (GMES), which aims to establish a European capacity for the provision and use of operational information for monitoring and management of the environment and civil security by 2008. This paper documents the data policies of the variety of information providers likely to be involved in GMES, identifies the obstacles and draws conclusions on ways to improve data policy coherence. It addresses the main policy issues associated with Earth observation data, as well as with other types of environmental data. 相似文献
45.
46.
B M Rabin J A Joseph W A Hunt T B Dalton S B Kandasamy A H Harris B Ludewigt 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1994,14(10):457-466
The relative behavioral effectiveness of heavy particles was evaluated. Using the taste aversion paradigm in rats, the behavioral toxicity of most types of radiation (including 20Ne and 40Ar) was similar to that of 60Co photons. Only 56Fe and 93Nb particles and fission neutrons were significantly more effective. Using emesis in ferrets as the behavioral endpoint, 56Fe particles and neutrons were again the most effective; however, 60Co photons were significantly more effective than 18 MeV electrons. These results suggest that LET does not completely predict behavioral effectiveness. Additionally, exposing rats to 10 cGy of 56Fe particles attenuated amphetamine-induced taste aversion learning. This behavior is one of a broad class of behaviors which depends on the integrity of the dopaminergic system and suggests the possibility of alterations in these behaviors following exposure to heavy particles in a space radiation environment. 相似文献
47.
Christoph R. Englert John M. Harlander Charles M. Brown Kenneth D. Marr Ian J. Miller J. Eloise Stump Jed Hancock James Q. Peterson Jay Kumler William H. Morrow Thomas A. Mooney Scott Ellis Stephen B. Mende Stewart E. Harris Michael H. Stevens Jonathan J. Makela Brian J. Harding Thomas J. Immel 《Space Science Reviews》2017,212(1-2):553-584
The Michelson Interferometer for Global High-resolution Thermospheric Imaging (MIGHTI) instrument was built for launch and operation on the NASA Ionospheric Connection Explorer (ICON) mission. The instrument was designed to measure thermospheric horizontal wind velocity profiles and thermospheric temperature in altitude regions between 90 km and 300 km, during day and night. For the wind measurements it uses two perpendicular fields of view pointed at the Earth’s limb, observing the Doppler shift of the atomic oxygen red and green lines at 630.0 nm and 557.7 nm wavelength. The wavelength shift is measured using field-widened, temperature compensated Doppler Asymmetric Spatial Heterodyne (DASH) spectrometers, employing low order échelle gratings operating at two different orders for the different atmospheric lines. The temperature measurement is accomplished by a multichannel photometric measurement of the spectral shape of the molecular oxygen A-band around 762 nm wavelength. For each field of view, the signals of the two oxygen lines and the A-band are detected on different regions of a single, cooled, frame transfer charge coupled device (CCD) detector. On-board calibration sources are used to periodically quantify thermal drifts, simultaneously with observing the atmosphere. The MIGHTI requirements, the resulting instrument design and the calibration are described. 相似文献
48.
49.
A. Nathues H. Boehnhardt A.W. Harris C. Jentsch S. Schaeff F. Weischede A. Wiegand N. Schmitz W. Goetz Z. Kachri 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
ASTEX (ASTeroid EXplorer) is a concept study of an in situ exploration mission to two Near-Earth-Asteroids (NEAs), which consists of an orbiting element and two individual lander units. The target candidates have different mineralogical compositions, i.e. one asteroid is chosen to be of “primitive’’ nature, the other to be a fragment of a differentiated asteroid. The main scientific goals of the ASTEX mission are the exploration of the physical, geological, and mineralogical nature of the NEAs. The higher level goal is the provision of information and constraints on the formation and evolution of our planetary system. The study identified realistic mission scenarios, defined the strawman payload as well as the requirements and options for the spacecraft bus including the propulsion system, the landers, the launcher, and assessed and defined the requirements for the mission’s operational ground segment. 相似文献
50.