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141.
使用一个全球原始方程半谱模式,模拟了行星波的跨赤道传播。结果指出:冬半球对流层顶附近准定常行星波的幅度起伏和相位变化,可以造成中层大气行星波的跨赤道传播,并且在夏半球形成瞬变行星波。所得结果为中层大气行星波的跨赤道传播、夏半球行星波的形成和南北半球之间的耦合提供了一种物理机制。 相似文献
142.
介绍了一种新型对称加载行星牵引传动减速器,它保留了行星齿轮传动比大的优点.由于它采用3组行星轮与2个锥面钢套对称加载,利用牵引油拖动,工作面多,传动效率高;接触处采用共曲面,接触应力下降;与齿轮传动相比结构简单,制造安装方便,噪声小,特别具有不受行星齿轮传动齿数安装条件限制的优点. 相似文献
143.
144.
The chemical composition of comet nuclei derived from current data on interstellar dust ingredients and comet dust and coma
molecules are shown to be substantially consistent with each other in both refractory and volatile components. When limited
by relative cosmic abundances the water in comet nuclei is constrained to be close to 30% by mass and the refractory to volatile
ratio is close to 1:1. The morphological structure of comet nuclei, as deduced from comet dust infrared continuum and spectral
emission properties, is described by a fluffy (porous) aggregate of tenth micron silicate core-organic refractory mantle particle
on which outer mantles of predominantly H2O ices contain embedded carbonaceous and polycyclic aromatic hydrocarbon (PAH) type particles of size in the of 1 - 10nm range.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
145.
Zoe A. Landsman Cody D. Schultz Daniel T. Britt Makayla Peppin Ryan L. Kobrick Philip T. Metzger Nina Orlovskaya 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(10):3308-3327
The Martian moon Phobos is the target of the upcoming JAXA Martian Moons eXploration (MMX) mission. There are currently no known samples of Phobos, so spacecraft hardware testing and scientific studies require Phobos regolith simulants. Here, we present two new Phobos regolith simulants: Phobos Captured Asteroid-1 (PCA-1) and Phobos Giant Impact (PGI-1). These two simulants reflect the two hypotheses for Phobos’s formation, and thus the two broad possibilities for composition. This work follows previous efforts to document the development of mineralogically accurate simulants, in an effort to overcome past pitfalls with inappropriate uses of simulants. We report physical and geotechnical properties of PCA-1 and PGI-1, including their reflectance spectra, grain size distributions, abrasivity, cohesion, strength, and hardness. Our intent is for PCA-1 and PGI-1 to be open standards for Phobos simulants, and we present the simulant recipes and production methodology for use and modification by the community. 相似文献
146.
Dmitriy Korotyshkin Eugeny Merzlyakov Christoph Jacobi Friederike Lilienthal Qian Wu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(10):3154-3166
The mid-latitude mesosphere and lower thermosphere (MLT) wind speeds measured by two SKiYMET meteor radars (MRs) at Collm (51°N, 13°E) and Kazan (56°N, 49°E) during 2016–2017 were analyzed to study longitudinal wind structures. The differences between monthly mean prevailing wind speeds and tidal amplitudes were compared with the corresponding differences obtained from TIMED/TIDI satellite winds and gradient wind speeds from the AURA/MLS instrument. It is shown that the MR wind difference between the two sites is statistically significant. The difference of the horizontal prevailing winds can be explained by a superposition of the background zonal flow, which is different at the two latitudes, with stationary planetary waves of different origin. Non-migrating tides contribute significantly to the difference of the semidiurnal tidal winds between the two sites. 相似文献
147.
基于多目标管理方法,阐述了玉兔号巡视器定位多目标管理的概念。兼顾技术成熟度、定位效率、冗余验证和阶段化分层管理等原则,对玉兔号巡视器着陆点和导航点的定位方法进行建模及分析比较,给出对应的定位方案。最后,将基于此多目标管理方法制定的方案,应用于玉兔号巡视器的定位任务,定位精度优于亚像素级,相对定位精度优于4%。 相似文献
148.
The James Webb Space Telescope 总被引:4,自引:0,他引:4
Jonathan P. Gardner John C. Mather Mark Clampin Rene Doyon Matthew A. Greenhouse Heidi B. Hammel John B. Hutchings Peter Jakobsen Simon J. Lilly Knox S. Long Jonathan I. Lunine Mark J. Mccaughrean Matt Mountain John Nella George H. Rieke Marcia J. Rieke Hans-Walter Rix Eric P. Smith George Sonneborn Massimo Stiavelli H. S. Stockman Rogier A. Windhorst Gillian S. Wright 《Space Science Reviews》2006,123(4):485-606
The James Webb Space Telescope (JWST) is a large (6.6 m), cold (<50 K), infrared (IR)-optimized space observatory that will be launched early in the next decade into orbit around the second Earth–Sun Lagrange point. The observatory will have four instruments: a near-IR camera, a near-IR multiobject spectrograph, and a tunable filter imager will cover the wavelength range, 0.6 < ; < 5.0 μ m, while the mid-IR instrument will do both imaging and spectroscopy from 5.0 < ; < 29 μ m.The JWST science goals are divided into four themes. The key objective of The End of the Dark Ages: First Light and Reionization theme is to identify the first luminous sources to form and to determine the ionization history of the early universe. The key objective of The Assembly of Galaxies theme is to determine how galaxies and the dark matter, gas, stars, metals, morphological structures, and active nuclei within them evolved from the epoch of reionization to the present day. The key objective of The Birth of Stars and Protoplanetary Systems theme is to unravel the birth and early evolution of stars, from infall on to dust-enshrouded protostars to the genesis of planetary systems. The key objective of the Planetary Systems and the Origins of Life theme is to determine the physical and chemical properties of planetary systems including our own, and investigate the potential for the origins of life in those systems. Within these themes and objectives, we have derived representative astronomical observations.To enable these observations, JWST consists of a telescope, an instrument package, a spacecraft, and a sunshield. The telescope consists of 18 beryllium segments, some of which are deployed. The segments will be brought into optical alignment on-orbit through a process of periodic wavefront sensing and control. The instrument package contains the four science instruments and a fine guidance sensor. The spacecraft provides pointing, orbit maintenance, and communications. The sunshield provides passive thermal control. The JWST operations plan is based on that used for previous space observatories, and the majority of JWST observing time will be allocated to the international astronomical community through annual peer-reviewed proposal opportunities. 相似文献
149.
徐焕然 《中国民航学院学报》1992,10(1):58-64
本文根据航空发动机和动力传动系统减速器的特点,提出了常用的NGW型行星减速器设计是“机械设计”课程设计的最佳题目。扼要分析了其计算特点和结构特点,并给出了设计题目及部分原始数据以供参考。 相似文献
150.