全文获取类型
收费全文 | 88篇 |
免费 | 1篇 |
国内免费 | 3篇 |
专业分类
航空 | 34篇 |
航天技术 | 24篇 |
航天 | 34篇 |
出版年
2024年 | 1篇 |
2021年 | 4篇 |
2019年 | 1篇 |
2018年 | 4篇 |
2017年 | 2篇 |
2015年 | 3篇 |
2014年 | 2篇 |
2013年 | 9篇 |
2012年 | 6篇 |
2011年 | 4篇 |
2010年 | 7篇 |
2009年 | 5篇 |
2008年 | 5篇 |
2007年 | 8篇 |
2006年 | 5篇 |
2005年 | 5篇 |
2004年 | 3篇 |
2003年 | 4篇 |
2002年 | 2篇 |
1999年 | 1篇 |
1998年 | 1篇 |
1997年 | 1篇 |
1996年 | 1篇 |
1995年 | 1篇 |
1987年 | 1篇 |
1986年 | 1篇 |
1985年 | 1篇 |
1975年 | 1篇 |
1967年 | 1篇 |
1966年 | 1篇 |
1965年 | 1篇 |
排序方式: 共有92条查询结果,搜索用时 62 毫秒
41.
Christopher S. Reynolds 《Space Science Reviews》2014,183(1-4):277-294
I review the current status of X-ray reflection (a.k.a. broad iron line) based black hole spin measurements. This is a powerful technique that allows us to measure robust black hole spins across the mass range, from the stellar-mass black holes in X-ray binaries to the supermassive black holes in active galactic nuclei. After describing the basic assumptions of this approach, I lay out the detailed methodology focusing on “best practices” that have been found necessary to obtain robust results. Reflecting my own biases, this review is slanted towards a discussion of supermassive black hole (SMBH) spin in active galactic nuclei (AGN). Pulling together all of the available XMM-Newton and Suzaku results from the literature that satisfy objective quality control criteria, it is clear that a large fraction of SMBHs are rapidly-spinning, although there are tentative hints of a more slowly spinning population at high (M>5×107 M ⊙) and low (M<2×106 M ⊙) mass. I also engage in a brief review of the spins of stellar-mass black holes in X-ray binaries. In general, reflection-based and continuum-fitting based spin measures are in agreement, although there remain two objects (GRO J1655–40 and 4U 1543–475) for which that is not true. I end this review by discussing the exciting frontier of relativistic reverberation, particularly the discovery of broad iron line reverberation in XMM-Newton data for the Seyfert galaxies NGC 4151, NGC 7314 and MCG–5-23-16. As well as confirming the basic paradigm of relativistic disk reflection, this detection of reverberation demonstrates that future large-area X-ray observatories such as LOFT will make tremendous progress in studies of strong gravity using relativistic reverberation in AGN. 相似文献
42.
Christopher Kebschull Sven Kevin Flegel Vitali BraunJohannes Gelhaus Marek MöckelCarsten Wiedemann Peter Vörsmann 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Within the last year three major re-entries occurred. The satellites UARS, ROSAT and Phobos-Grunt entered Earth’s atmosphere with fragments reaching the surface. Due to a number of uncertainties in propagating an object’s trajectory the exact place and time of a satellite’s re-entry is hard to determine. Major influences when predicting the re-entry time are the changing precision of the available orbital data, the satellite’s ballistic coefficient, the activity of the sun which influences the Earth’s atmosphere and the underlying quality of the atmospheric model. In this paper a method is presented which can reduce the variability in short-term orbital lifetime prediction induced by fluctuating orbital data accuracies. A re-entry campaign is used as a reference for this purpose. For a window of a few weeks before the re-entry the position data of a synthetic object is disturbed considering different degrees of orbital data errors. As a result different predictions will exist for the generated position data of a given day. Using a regression algorithm on the available data an average position is obtained, which is then used for the orbital lifetime prediction. The effect of this measure is a more consistent prediction of the orbital lifetime. The paper concludes with the comparison of the generated re-entry windows in various test cases for the original and the averaged data. 相似文献
43.
44.
Nicholson WL Ricco AJ Agasid E Beasley C Diaz-Aguado M Ehrenfreund P Friedericks C Ghassemieh S Henschke M Hines JW Kitts C Luzzi E Ly D Mai N Mancinelli R McIntyre M Minelli G Neumann M Parra M Piccini M Rasay RM Ricks R Santos O Schooley A Squires D Timucin L Yost B Young A 《Astrobiology》2011,11(10):951-958
We report the first telemetered spaceflight science results from the orbiting Space Environment Survivability of Living Organisms (SESLO) experiment, executed by one of the two 10?cm cube-format payloads aboard the 5.5?kg Organism/Organic Exposure to Orbital Stresses (O/OREOS) free-flying nanosatellite. The O/OREOS spacecraft was launched successfully to a 72° inclination, 650?km Earth orbit on 19 November 2010. This satellite provides access to the radiation environment of space in relatively weak regions of Earth's protective magnetosphere as it passes close to the north and south magnetic poles; the total dose rate is about 15 times that in the orbit of the International Space Station. The SESLO experiment measures the long-term survival, germination, and growth responses, including metabolic activity, of Bacillus subtilis spores exposed to the microgravity, ionizing radiation, and heavy-ion bombardment of its high-inclination orbit. Six microwells containing wild-type (168) and six more containing radiation-sensitive mutant (WN1087) strains of dried B. subtilis spores were rehydrated with nutrient medium after 14 days in space to allow the spores to germinate and grow. Similarly, the same distribution of organisms in a different set of microwells was rehydrated with nutrient medium after 97 days in space. The nutrient medium included the redox dye Alamar blue, which changes color in response to cellular metabolic activity. Three-color transmitted intensity measurements of all microwells were telemetered to Earth within days of each of the 48?h growth experiments. We report here on the evaluation and interpretation of these spaceflight data in comparison to delayed-synchronous laboratory ground control experiments. 相似文献
45.
Valerie C. Thomas Joseph M. Makowski G. Mark Brown John F. McCarthy Dominick Bruno J. Christopher Cardoso W. Michael Chiville Thomas F. Meyer Kenneth E. Nelson Betina E. Pavri David A. Termohlen Michael D. Violet Jeffrey B. Williams 《Space Science Reviews》2011,163(1-4):175-249
The Dawn spacecraft is designed to travel to and operate in orbit around the two largest main belt asteroids, Vesta and Ceres. Developed to meet a ten-year life and fully redundant, the spacecraft accommodates an ion propulsion system, including three ion engines and xenon propellant tank, utilizes large solar arrays to power the engines, carries the science instrument payload, and hosts the hardware and software required to successfully collect and transmit the scientific data back to Earth. The launch of the Dawn spacecraft in September 2007 from Cape Canaveral Air Force Station was the culmination of nearly five years of design, development, integration and testing of this unique system, one of the very few scientific spacecraft to rely on ion propulsion. The Dawn spacecraft arrived at its first destination, Vesta, in July 2011, where it will conduct science operations for twelve months before departing for Ceres. 相似文献
46.
Jacobs R. Christopher H. Hamlen R. Rizzo R. Paur R. Gilman S. 《Aerospace and Electronic Systems Magazine, IEEE》1996,11(6):19-25
This paper describes the US Army's future needs for silent portable power in the area of batteries and fuel cells. These needs will continue to increase as a result of the introduction of newer types of equipment, the increasing digitization of the battlefield, and future integrated Soldier Systems. Current battery programs are aimed at improved, low-cost primary batteries, and rechargeable batteries with increased energy densities. The Army fuel cell program aimed at portable systems capable of the order of 150 W is also described 相似文献
47.
Anthony R. Yeates Tahar Amari Ioannis Contopoulos Xueshang Feng Duncan H. Mackay Zoran Mikić Thomas Wiegelmann Joseph Hutton Christopher A. Lowder Huw Morgan Gordon Petrie Laurel A. Rachmeler Lisa A. Upton Aurelien Canou Pierre Chopin Cooper Downs Miloslav Druckmüller Jon A. Linker Daniel B. Seaton Tibor Török 《Space Science Reviews》2018,214(5):99
Seven different models are applied to the same problem of simulating the Sun’s coronal magnetic field during the solar eclipse on 2015 March 20. All of the models are non-potential, allowing for free magnetic energy, but the associated electric currents are developed in significantly different ways. This is not a direct comparison of the coronal modelling techniques, in that the different models also use different photospheric boundary conditions, reflecting the range of approaches currently used in the community. Despite the significant differences, the results show broad agreement in the overall magnetic topology. Among those models with significant volume currents in much of the corona, there is general agreement that the ratio of total to potential magnetic energy should be approximately 1.4. However, there are significant differences in the electric current distributions; while static extrapolations are best able to reproduce active regions, they are unable to recover sheared magnetic fields in filament channels using currently available vector magnetogram data. By contrast, time-evolving simulations can recover the filament channel fields at the expense of not matching the observed vector magnetic fields within active regions. We suggest that, at present, the best approach may be a hybrid model using static extrapolations but with additional energization informed by simplified evolution models. This is demonstrated by one of the models. 相似文献
48.
Christopher W. Barnes 《Space Science Reviews》1985,42(1-2):145-151
It is usually important to write plasma simulation codes in such a way that they execute efficiently and are convenient to
use. I discuss here practical techniques to achieve this goal. Numerical algorithms must be well formulated and advantage
taken of machine architecture in casting the algorithm into a high level language such as Fortran. The advantages of writing
critical routines in Assembler are discussed. For large simulation codes, disks must often be used as a temporary store for
working data. Efficient methods for doing this are presented. Codes must not only be well organized for ease of implementation
and maintenance, but also for ease of use. Ways are suggested for packaging codes such that setup, batch production, restarting
and diagnostic postprocessing is facilitated. Particular emphasis is placed on graphics postprocessors, since they must be
used in real time with graphics terminals as well as with hardcopy devices. 相似文献
49.
Christopher J. Mertens James M. Russell III Martin G. Mlynczak Chiao-Yao She Francis J. Schmidlin Richard A. Goldberg Manuel López-Puertas Peter P. Wintersteiner Richard H. Picard Jeremy R. Winick Xiaojing Xu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The Sounding of the Atmosphere using Broadband Emission Radiometry (SABER) experiment is one of four instruments on NASA’s Thermosphere–Ionosphere–Energetics and Dynamics (TIMED) satellite. SABER measures broadband infrared limb emission and derives vertical profiles of kinetic temperature (Tk) from the lower stratosphere to approximately 120 km, and vertical profiles of carbon dioxide (CO2) volume mixing ratio (vmr) from approximately 70 km to 120 km. In this paper we report on SABER Tk/CO2 data in the mesosphere and lower thermosphere (MLT) region from the version 1.06 dataset. The continuous SABER measurements provide an excellent dataset to understand the evolution and mechanisms responsible for the global two-level structure of the mesopause altitude. SABER MLT Tk comparisons with ground-based sodium lidar and rocket falling sphere Tk measurements are generally in good agreement. However, SABER CO2 data differs significantly from TIME-GCM model simulations. Indirect CO2 validation through SABER-lidar MLT Tk comparisons and SABER-radiation transfer comparisons of nighttime 4.3 μm limb emission suggest the SABER-derived CO2 data is a better representation of the true atmospheric MLT CO2 abundance compared to model simulations of CO2 vmr. 相似文献
50.
Helene L. Winters Deborah L. Domingue Teck H. Choo Raymond Espiritu Christopher Hash Erick Malaret Alan A. Mick Joseph P. Skura Joshua Steele 《Space Science Reviews》2007,131(1-4):601-623
The MESSENGER Science Operations Center (SOC) is an integrated set of subsystems and personnel whose purpose is to obtain,
provide, and preserve the scientific measurements and analysis that fulfill the objectives of the MErcury Surface, Space ENvironment,
GEochemistry, and Ranging (MESSENGER) mission. The SOC has two main functional areas. The first is to facilitate science instrument
planning and operational activities, including related spacecraft guidance and control operations, and to work closely with
the Mission Operations Center to implement those plans. The second functional area, data management and analysis, involves
the receipt of science-related telemetry, reformatting and cataloging this telemetry and related ancillary information, retaining
the science data for use by the MESSENGER Science Team, and preparing data archives for delivery to the Planetary Data System;
and the provision of operational assistance to the instrument and science teams in executing their algorithms and generating
higher-level data products. 相似文献