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641.
642.
We present a preliminary analysis of two quiet Sun transition region areas observed with the SOHO/SUMER spectrometer, using
lines from oxygen, nitrogen and silicon. The average quiet Sun physical parameters are studied as a function of line intensity.
Systematic variations of line position and width with increasing intensity are found. A large number of small-scale active
points have been observed, and preliminary analysis of the physical properties and dynamics of these active features is presented.
A jet-like structure, found in an active point, is also investigated and its velocity along the line of sight determined.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
643.
P. Lemaire 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2007,39(12):1876-1881
The two XUV–EUV spectrometers on SOHO have collected a large amount of data in the 6000–106 K solar plasma temperature range. These data have allowed us to greatly enhance our knowledge of the processes acting in the solar atmosphere, from the chromosphere to the corona. Some results on the quiet Sun structure (network, quiet Sun versus coronal hole), on the dynamics (velocities, waves, transient events), and the main characteristics of the quiet Sun atmosphere are presented and discussed. 相似文献
644.
飞船返回地球时再入速度很大,过大的过载和气动加热率尤其对载人飞船带来安全性问题。如果利用航天器在大气层外及其边缘处多次再入运动,可降低速度、耗散热量。文章主要分析了载人飞船在大气层外多次再入飞行时的各主要参数对飞船轨道和轨道终点的影响。在分析过程中,首先建立了飞船在大气层外飞行的数学模型,进而通过大量的数值仿真得到一条基准轨道,在此基础上分别改变轨道起始点参数(倾角、偏航角和飞行速度)的初始值,分析轨道的特性及轨道的终点误差。最后根据起始点参数值和对应的轨道终点误差值的关系,得到了飞船在大气层外飞行时的起始参数对飞行轨道及轨道终点影响的敏感度,从而为工程上轨道的设计提供一个有效的参考依据。 相似文献
645.
30CrMnSiA钢管外圆磁力研磨工艺的研究 总被引:1,自引:0,他引:1
采用化学粘结Fe+SiC磁性料对30CrMnSiA钢管外圆进行磁力研磨试验,研究了磨料成分、粒度以及研磨时间与研磨后表面粗糙度的关系,试验所得到的研磨表面粗糙度达到了Ra0.05μm。 相似文献
646.
R. Hollmann R.W. Mueller A. Gratzki 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2006,37(12):2166-II
In the phase of redefinition of the EUMETSAT ground segment seven so called Satellite Application Facilities (SAF) each of them serving dedicated user groups have been established in Europe. The SAF on climate monitoring (CM-SAF) will deliver a comprehensive set of climate variables, including from different cloud products, radiation budget at the top of the atmosphere, surface radiation budget and tropospheric humidity. A consistent dataset of cloud and radiation products in a high spatial resolution on a uniform grid is derived. The CM-SAF is a joint project of the German Meteorological Service, EUMETSAT and five other European Meteorological Services. It is dedicated to produce climate datasets using data from instruments onboard of METEOSAT Second Generation and polar orbiting satellites NOAA and METOP. After the development phase, the CM-SAF has started its initial operational phase in the end of 2003. In this context, the algorithms have been implemented at the processing centres and the processing of satellite data from the polar orbiting satellites of NOAA has commenced. This paper gives an overview of the first products of surface radiative fluxes and their validation with selected surface sites. 相似文献
647.
Magneto-gravity Waves Trapped in the Lower Solar Corona 总被引:1,自引:0,他引:1
Yu-Qing Lou 《Space Science Reviews》1999,87(1-2):261-264
The possibility of trapped magneto-gravity waves in the lower solar corona with an open magnetic field is discussed. Intensity
variations and/or Doppler shifts of relevant UV, EUV and x-ray spectral lines in the chromosphere, transition region and lower
corona may reveal the existence of such low-frequency modes (with periods longer than ∼ 1.5 hour). The spectrum may be either
discrete or continuous depending on the reflection property of the narrow transition region. These modes can be utilized to
probe the dynamics of the upper chromosphere, transition region and lower corona; they may also play an important role in
coronal heating.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
648.
编制捷联姿态解算软件是捷联惯性姿态参考系统研制中的重要一环。由于对计算的实时性和精度都有较高的要求,又在专用的弹上计算机上进行,所以增加了制作的难度。从变量取值范围、比例因子确定、字长选择、程序结构等几方面介绍了捷联姿态解算软件的编制情况。该软件是在导弹计算机上用TMS320C25宏汇编语言编制的。该软件经过地面实物试验,验证了其正确性。 相似文献
649.
对卫星表面材料的体电阻率、面电阻率的测试方法进行了研究,并设计了测量电极系统,测量了常用热控涂层的体、面电阻率,研究了测量电压对测量结果的影响。 相似文献
650.