全文获取类型
收费全文 | 294篇 |
免费 | 1篇 |
国内免费 | 2篇 |
专业分类
航空 | 152篇 |
航天技术 | 116篇 |
综合类 | 4篇 |
航天 | 25篇 |
出版年
2018年 | 8篇 |
2017年 | 2篇 |
2016年 | 2篇 |
2014年 | 9篇 |
2013年 | 11篇 |
2012年 | 3篇 |
2011年 | 12篇 |
2010年 | 4篇 |
2009年 | 13篇 |
2008年 | 18篇 |
2007年 | 9篇 |
2006年 | 17篇 |
2005年 | 7篇 |
2004年 | 5篇 |
2003年 | 15篇 |
2002年 | 3篇 |
2001年 | 9篇 |
2000年 | 8篇 |
1999年 | 10篇 |
1998年 | 6篇 |
1997年 | 4篇 |
1996年 | 6篇 |
1995年 | 3篇 |
1994年 | 8篇 |
1993年 | 5篇 |
1992年 | 7篇 |
1990年 | 3篇 |
1989年 | 6篇 |
1988年 | 5篇 |
1986年 | 2篇 |
1985年 | 6篇 |
1984年 | 9篇 |
1983年 | 1篇 |
1982年 | 8篇 |
1981年 | 14篇 |
1980年 | 2篇 |
1979年 | 1篇 |
1978年 | 3篇 |
1977年 | 4篇 |
1976年 | 6篇 |
1975年 | 2篇 |
1974年 | 1篇 |
1973年 | 1篇 |
1972年 | 5篇 |
1971年 | 2篇 |
1970年 | 3篇 |
1969年 | 1篇 |
1967年 | 2篇 |
1964年 | 1篇 |
1962年 | 1篇 |
排序方式: 共有297条查询结果,搜索用时 140 毫秒
251.
H. U. Auster I. Apathy G. Berghofer A. Remizov R. Roll K. H. Fornacon K. H. Glassmeier G. Haerendel I. Hejja E. Kührt W. Magnes D. Moehlmann U. Motschmann I. Richter H. Rosenbauer C. T. Russell J. Rustenbach K. Sauer K. Schwingenschuh I. Szemerey R. Waesch 《Space Science Reviews》2007,128(1-4):221-240
The scientific objectives, design and capabilities of the Rosetta Lander’s ROMAP instrument are presented. ROMAP’s main scientific
goals are longterm magnetic field and plasma measurements of the surface of Comet 67P/Churyumov-Gerasimenko in order to study
cometary activity as a function of heliocentric distance, and measurements during the Lander’s descent to investigate the
structure of the comet’s remanent magnetisation. The ROMAP fluxgate magnetometer, electrostatic analyser and Faraday cup measure
the magnetic field from 0 to 32 Hz, ions of up to 8000 keV and electrons of up to 4200 keV. Additional two types of pressure
sensors – Penning and Minipirani – cover a pressure range from 10−8 to 101 mbar. ROMAP’s sensors and electronics are highly integrated, as required by a combined field/plasma instrument with less
than 1 W power consumption and 1 kg mass. 相似文献
252.
The THEMIS Magnetic Cleanliness Program 总被引:1,自引:0,他引:1
M. Ludlam V. Angelopoulos E. Taylor R. C. Snare J. D. Means Y. S. Ge P. Narvaez H. U. Auster O. Le Contel D. Larson T. Moreau 《Space Science Reviews》2008,141(1-4):171-184
The five identical THEMIS Spacecraft, launched in February 2007, carry two magnetometers on each probe, one DC fluxgate (FGM) and one AC search coil (SCM). Due to the small size of the THEMIS probes, and the short length of the magnetometer booms, magnetic cleanliness was a particularly complex task for this medium sized mission. The requirements leveled on the spacecraft and instrument design required a detailed approach, but one that did not hamper the development of the probes during their short design, production and testing phase. In this paper we describe the magnetic cleanliness program’s requirements, design guidelines, program implementation, mission integration and test philosophy and present test results, and mission on-orbit performance. 相似文献
253.
254.
The solar upper atmosphere (SUA) is defined as the volume above the photosphere occupied by plasmas with electron temperatures, T
e, above 2×104 K. Until the Skylab era, only little was known about the morphology of the SUA, while the quality of the spectroscopic observations was continually improving. A spherically symmetric atmosphere was assumed at that time, in which the temperature increased with height. With advances in the observational techniques, it became apparent that the morphology of the SUA was very complex even during the minimum of the magnetic activity cycle. In particular, spectroscopic measurements with high spectral and spatial resolution, which were made in the light of ultraviolet emission lines representing a variety of temperatures, led to the conclusion that most of the radiation from the solar transition region could not be explained by assuming a continuous chromosphere-corona interface, but rather by a region of unresolved fine structures. Recent observational results obtained by modern instruments, such as the Extreme-ultraviolet Imaging Telescope (EIT), the Large Angle Spectroscopic Coronagraph (LASCO), and the Solar Ultraviolet Measurements of (SUMER) spectrograph on the Solar and Heliospheric Observatory (SOHO), as well as the Transition Region and Coronal Explorer (TRACE), and their interpretations will be presented in this review of our understanding of the morphology of the SUA. 相似文献
255.
Chiu M.C. Von-Mehlem U.I. Willey C.E. Betenbaugh T.M. Maynard J.J. Krein J.A. Conde R.F. Gray W.T. Hunt J.W. Mosher L.E. McCullough M.G. Panneton P.E. Staiger J.P. Rodberg E.H. 《Space Science Reviews》1998,86(1-4):257-284
The Johns Hopkins University Applied Physics Laboratory (JHU/APL) was responsible for the design and fabrication of the ACE
spacecraft to accommodate the ACE Mission requirements and for the integration, test, and launch support for the entire ACE
Observatory. The primary ACE Mission includes a significant number of science instruments - nine - whose diverse requirements
had to be factored into the overall spacecraft bus design. Secondary missions for monitoring space weather and measuring launch
vibration environments were also accommodated within the spacecraft design. Substantial coordination and cooperation were
required between the spacecraft and instrument engineers, and all requirements were met. Overall, the spacecraft was kept
as simple as possible in meeting requirements to achieve a highly reliable and low-cost design.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
256.
运用ANSYS CFX 11.0和home-code程序对AI222发动机风扇流路气动参数进行了3维CFD(Computational Fluid Dynamics)计算;通过3维建模,实现了风扇主要积分特性和局部参数计算。通过与风扇进行大量试验结果的对比,验证了计算结果,并找出了产生差别的原因,得到了风扇总特性以及气流径向参数的计算值与试验值的吻合度。结果表明:通过运用3维建模计算方法简化了风扇设计过程,缩短了风扇从设计到试验的时间,降低了航空发动机部件的设计成本。 相似文献
257.
C.J. Rodriguez-Solano U. HugentoblerP. Steigenberger G. Allende-Alba 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
During Sun-Earth eclipse seasons, GPS-IIA satellites perform noon, shadow and post-shadow yaw maneuvers. If the yaw maneuvers are not properly taken into account in the orbit determination process, two problems appear: (1) the observations residuals increase since the modeled position of the satellite’s navigation antenna differs from the true position, and (2) the non-conservative forces like solar radiation pressure or Earth radiation pressure are mismodeled due to the wrong orientation of the satellite’s surfaces in space. 相似文献
258.
The Dawn Framing Camera 总被引:1,自引:0,他引:1
H. Sierks H. U. Keller R. Jaumann H. Michalik T. Behnke F. Bubenhagen I. B��ttner U. Carsenty U. Christensen R. Enge B. Fiethe P. Guti��rrez Marqu��s H. Hartwig H. Kr��ger W. K��hne T. Maue S. Mottola A. Nathues K.-U. Reiche M. L. Richards T. Roatsch S. E. Schr?der I. Szemerey M. Tschentscher 《Space Science Reviews》2011,163(1-4):263-327
The Framing Camera (FC) is the German contribution to the Dawn mission. The camera will map 4 Vesta and 1 Ceres through a clear filter and 7 band-pass filters covering the wavelengths from the visible to the near-IR. The camera will allow the determination of the physical parameters of the asteroids, the reconstruction of their global shape as well as local topography and surface geomorphology, and provide information on composition via surface reflectance characteristics. The camera will also serve for orbit navigation. The resolution of the Framing Camera will be up to 12 m per pixel in low altitude mapping orbit at Vesta (62 m per pixel at Ceres), at an angular resolution of 93.7 ??rad?px?1. The instrument uses a reclosable front door to protect the optical system and a filter-wheel mechanism to select the band-pass for observation. The detector data is read out and processed by a data processing unit. A power converter unit supplies all required power rails for operation and thermal maintenance. For redundancy reasons, two identical cameras were provided, both located side by side on the +Z-deck of the spacecraft. Each camera has a mass of 5.5 kg. 相似文献
259.
P. Jakobsson D. Malesani J. Hjorth J.P.U. Fynbo B. Milvang-Jensen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
We describe the current status and recent results from our Swift/VLT legacy survey, a VLT Large Programme aimed at characterizing the host galaxies of a homogeneously selected sub-sample of Swift GRBs. The immediate goals are to determine the host luminosity function, study the effects of reddening, determine the fraction of Lyα emitters in the hosts, and obtain redshifts for targets without a reported one. The main effort so far has been the definition of a very carefully selected sample, obeying strict and well-defined criteria: 68 targets in total. Among the preliminary results is a large optical detection rate, the lack of extremely red objects (only one possible case in the sample) and an update of the Swift GRB redshift distribution with 〈z〉∼2.0. 相似文献
260.
R Anken M Ibsch U Kniesel H Rahmann 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,33(8):1411-1415
The origin of the proteinacious matrix of the inner ear stones (otoliths) of vertebrates has not yet been clarified. Using the backstroke mutant (bks) of the zebrafish Danio rerio, which is characterized by a complete lack of otoliths, we searched for possibly missing or aberrant structural components within the macular epithelia of the inner ears of embryos on the ultrastructural level. Numerous multilamellar bodies (MLBs) were found. The MLBs were, however, not restricted to the inner ears of mutants but were also found in wildtype individuals and in further organs such as brain and liver. MLBs have hitherto never been described from the inner ear of fish and are generally estimated to be rare structures. Their occurrence in fish liver can, however, be induced by using particular chemical substances, which seem to effect adaptive compensatory processes on the cellular level. Such a chemical treatment also affects the ultrastructure of further organelles. Since the occurrence of MLBs in the liver of zebrafish was not accompanied by an alteration of the morphology of other organelles, their occurrence seems not to be due to environmental stress. The findings indicate that the MLBs cannot be correlated with bks-inherent features as well as with missing otolith development/growth. Since the occurrence of MLBs was independent from the developmental stage of a specimen and its overall tissue preservation, it can moreover be excluded that these MLBs merely represent fixation artifacts. Their presence more likely indicates cellular remodelling processes of hitherto unknown significance. 相似文献