排序方式: 共有42条查询结果,搜索用时 15 毫秒
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Quantification of spatial structure of human proximal tibial bone biopsies using 3D measures of complexity 总被引:2,自引:0,他引:2
Saparin PI Thomsen JS Prohaska S Zaikin A Kurths J Hege HC Gowin W 《Acta Astronautica》2005,56(9-12):820-830
Changes in trabecular bone composition during development of osteoporosis are used as a model for bone loss in microgravity conditions during a space flight. Symbolic dynamics and measures of complexity are proposed and applied to assess quantitatively the structural composition of bone tissue from 3D data sets of human tibia bone biopsies acquired by a micro-CT scanner. In order to justify the newly proposed approach, the measures of complexity of the bone architecture were compared with the results of traditional 2D bone histomorphometry. The proposed technique is able to quantify the structural loss of the bone tissue and may help to diagnose and to monitor changes in bone structure of patients on Earth as well as of the space-flying personnel. 相似文献
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E. A. Gurtovenko R. I. Kostik A. Tlamicha R. Zerull Aert Schadee A. Mészáros Y. Néeman R. H. Giese A. T. Sinclair J. Kleczek E. A. Trendelenburg Wolfgang Hillebrandt L. Sehnal W. de Graaff C. Slottje T. Courvisier H. F. van Beek B. Baud C. de Jager J. M. A. Danby B. V. Somov J. Cassinelli F. Verbunt 《Space Science Reviews》1986,44(1-2):177-188
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Venus and Mars likely had liquid water bodies on their surface early in the Solar System history. The surfaces of Venus and Mars are presently not a suitable habitat for life, but reservoirs of liquid water remain in the atmosphere of Venus and the subsurface of Mars, and with it also the possibility of microbial life. Microbial organisms may have adapted to live in these ecological niches by the evolutionary force of directional selection. Missions to our neighboring planets should therefore be planned to explore these potentially life-containing refuges and return samples for analysis. Sample return missions should also include ice samples from Mercury and the Moon, which may contain information about the biogenic material that catalyzed the early evolution of life on Earth (or elsewhere). To obtain such information, science-driven exploration is necessary through varying degrees of mission operation autonomy. A hierarchical mission design is envisioned that includes spaceborne (orbital), atmosphere (airborne), surface (mobile such as rover and stationary such as lander or sensor), and subsurface (e.g., ground-penetrating radar, drilling, etc.) agents working in concert to allow for sufficient mission safety and redundancy, to perform extensive and challenging reconnaissance, and to lead to a thorough search for evidence of life and habitability. 相似文献
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With ongoing progress in space technology, questions of its potential for the modification of weather and climate phenomena (often summarized by the term ‘geoengineering’) ranging from small-scale severe weather events to mitigation of effects caused by global climate change and ozone depletion have become popular. This paper reviews the current state of scientifically based studies in this context and attempts to provide a basis for an assessment of geoengineering efforts with respect to technological, economic and fundamental scientific aspects. The overview indicates that the current state of knowledge about climate variability as a consequence of natural and anthropogenic influences is sufficient to classify geoengineering solutions as highly risky and their consequences as extremely difficult to predict. Even on smaller scales and with less complexity of interacting processes, only very limited boundary conditions, i.e. a narrow range of atmospheric variability and land surface topography favouring the intended alteration, seem to justify weather modification. Moreover, as for systems reaching scales of large organized storms and hurricanes, required energy and control resources are well beyond existing capabilities. Consequently, the use of space technology for provision of better information on environmental change and integration of remote sensing data into weather and climate models forecasts is supported. 相似文献
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Wolfgang Baumjohann Michel Blanc Andrei Fedorov Karl-Heinz Glassmeier 《Space Science Reviews》2010,152(1-4):99-134
The interaction of planets with the solar wind produces a diversity of current systems, yet these can be classified into only a few different types, which include ionospheric currents, currents carried by magnetospheric boundaries like the magnetopause or ionopause, magnetotail currents, and currents flowing inside the magnetospheres, like ring currents, plasma sheet currents and currents aligned to the magnetic field lines (or field-aligned currents). 相似文献
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Christoph Lotz Yvonne Wessarges Jörg Hermsdorf Wolfgang Ertmer Ludger Overmeyer 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(8):1967-1974
Through the striving of humanity into space, new production processes and technologies for the use under microgravity will be essential in the future. Production of objects in space demands for new processes, like additive manufacturing. This paper presents the concept and the realization for a new machine to investigate microgravity production processes on earth. The machine is based on linear long stator drives and a vacuum chamber carrying up to 1000?kg. For the first time high repetition rate and associated low experimental costs can provide basic research. The paper also introduces the substrate-free additive manufacturing as a future research topic and one of our primary application. 相似文献
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Chaboche热粘塑性损伤模型的应用研究 总被引:1,自引:1,他引:1
本文讨论了Chaboche粘塑性模型的材料参数确定问题,提出了一种简单实用的模型参数确定方法,并用本文提出的方法确定了TiAl材料的Chaboche模型参数,并用这些参数进行了不同应变率下的拉伸模拟计算、不同应力下的蠕变模拟计算和CT试样在阶梯载荷下的蠕变模拟计算。 相似文献
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Patric Seefeldt Jan Thimo Grundmann Martin Hillebrandt Martin Zander 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2736-2745
For precursor solar sail activities a strategy for a controlled deployment of large membranes was developed based on a combination of zig-zag folding and coiling of triangular sail segments spanned between crossed booms. This strategy required four autonomous deployment units that were jettisoned after the deployment is completed. In order to reduce the complexity of the system an adaptation of that deployment strategy is investigated.A baseline design for the deployment mechanisms is established that allows the deployment actuation from a central bus system in order to reduce the complexity of the system. The mass of such a sail craft will be slightly increased but its performance is still be reasonable for first solar sail missions.The presented design will be demonstrated on breadboard level showing the feasibility of the deployment strategy. The characteristic acceleration will be evaluated and compared to the requirements of certain proposed solar sail missions. 相似文献