共查询到20条相似文献,搜索用时 578 毫秒
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A white light coronagraph was launched into orbit aboard the space shuttle OV 103 (Discovery) on 7 April 1993. This device was one of two instruments included in the SPARTAN 201-1 payload, a completely autonomous sub-satellite deployed from the shuttle for a period of about 47 hours. The WLC system is an externally occulted coronagraph system which incorporates a rotating half-wave plate polarimeter, and the image data is used to infer the brightness, the polarized brightness and the degree of polarization of the white light emission from the solar corona. These data are in turn used to infer estimates of the K- and F-coronal brightnesses and density distributions. We shall present preliminary results of the electron density estimate in the coronal streamer and hole region and describe the methods employed.affiliated to USRA 相似文献
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J. L. Kohl L. D. Gardner L. Strachan R. Fisher M. Guhathakurta 《Space Science Reviews》1995,72(1-2):29-38
Spartan 201 is a shuttle deployed spacecraft that is scheduled to perform ultraviolet spectroscopy and white light polarimetry of the extended solar corona during two 40 hour missions to occur in September 1994 and August 1995. The spectroscopy is done with an ultraviolet coronal spectrometer which measures the intensity and spectral line profile of HI Ly up to heliocentric heights of 3.5 solar radii. It also measures the intensities of the OVI doublet at 1032 and 1037 Å and of Fe XII at 1242 Å. The HI Ly line profile measurements are used to determine the random velocity distribution of coronal protons along the line-of-sight. The absolute HI Ly intensities can be used together with electron densities from the white light coronagraph to estimate electron temperatures from hydrogen ionization balance calculations, and bulk outflow velocities from models of Doppler dimmed resonant scattering. Intensities of minor ion lines are used to determine coronal abundances and outflow velocities of O5+. Ultraviolet spectroscopy of extended coronal regions from the 11 April 1993 mission of Spartan 201 are discussed. 相似文献
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采用近液相线铸造的方法制备出ZL201合金半固态锭坯,并对其进行了触变挤压成形,利用金相显微镜观察r其组织变化,并与常规铸造ZL201合金的组织与挤压成形件的组织进行了对比分析.研究结果表明:(1)半固态合金挤压后组织更细小均匀,消除了宏观偏析、晶内疏松等问题,有利于性能的提高.(2)半固态挤压组织更细小均匀的主要原因是在挤压过程中晶粒的变形量、畸变区域很大,故在动态再结晶的过程中,半固态合金转变的体积分数大于常规铸造合金,所以半同态合金挤压件组织更加细小均匀. 相似文献
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The instruments on the Spartan 201 spacecraft are an Ultraviolet Coronal Spectrometer and a White Light Coronagraph. Spartan 201 was deployed by the Space Shuttle on 11 April 1993 and observed the extended solar corona for about 40 hours. The Ultraviolet Coronal Spectrometer measured the intensity and spectral line profile of HI Ly and the intensities of OVI 103.2 and 103.7 nm. Observations were made at heliocentric heights between 1.39 and 3.5 R. Four coronal targets were observed, a helmet streamer at heliographic position angle 135°, the north and south polar coronal holes, and an active region above the west limb. Measurements of the HI Ly geocorona and the solar irradiance were also made. The instrument performed as expected. Straylight suppression, spectral focus, radiometric sensitivity and background levels all appear to be satisfactory. The uv observations are aimed at determining proton temperatures and outflow velocities of hydrogen, protons and oxygen ions. Preliminary results from the north polar coronal hole observations are discussed. 相似文献
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综合航空电子系统对其内部的各个功能模块提出了应用数据集中存储,实时重构等要求,具有动态重载功能的信号处理模块能极大提高系统的应用灵活性、可靠性和可维护性。为了适应这种需求,通过分析ADSP-TS201S处理器几种引导方式的原理和方法,提出了通过修改加载内核,并进行二次引导以实现动态加载的方案。该方案已结合ADSP-TS201S信号处理模块应用平台,在某处理机系统中获得了成功应用。 相似文献
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M. P. Miralles L. Strachan L. D. Gardner P. L. Smith J. L. Kohl M. Guhathakurta R. R. Fisher 《Space Science Reviews》1999,87(1-2):277-281
The Spartan 201 flights from 1993 to 1995 provided us with observations in H I Lyman-α of several coronal hole/streamer boundaries
and adjacent streamers during the declining phase of the current solar cycle: Analysis of the latitudinal dependence of the
line intensities clearly shows that there is a boundary region at the coronal hole/streamer interface where the H I Lyman-α
intensity reaches a minimum value. Similar results are also found in UVCS/SOHO observations. We also discuss differences in
the coronal hole/streamer boundaries for different types of streamers and their changes over the three year period of Spartan
201 observations.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
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Guhathakurta Madhullika Sittler Ed Fisher Richard Kucera Theresa Gibson Sarah McComas Dave Skoug Ruth 《Space Science Reviews》2001,97(1-4):45-50
The large-scale coronal magnetic fields of the Sun are believed to play an important role in organizing the coronal plasma
and channeling the high and low speed solar wind along the open magnetic field lines of the polar coronal holes and the rapidly
diverging field lines close to the current sheet regions, as has been observed by the instruments aboard the Ulysses spacecraft from March 1992 to March 1997. We have performed a study of this phenomena within the framework of a semi-empirical
model of the coronal expansion and solar wind using Spartan, SOHO, and Ulysses observations during the quiescent phase of the solar cycle. Key to this understanding is the demonstration that the white
light coronagraph data can be used to trace out the topology of the coronal magnetic field and then using the Ulysses data to fix the strength of the surface magnetic field of the Sun. As a consequence, it is possible to utilize this semi-empirical
model with remote sensing observation of the shape and density of the solar corona and in situ data of magnetic field and
mass flux to predict values of the solar wind at all latitudes through out the solar system. We have applied this technique
to the observations of Spartan 201-05 on 1–2 November, 1998, SOHO and Ulysses during the rising phase of this solar cycle and speculate on what solar wind velocities Ulysses will observe during its polar passes over the south and the north poles during September of 2000 and 2001. In order to do
this the model has been generalized to include multiple streamer belts and co-located current sheets. The model shows some
interesting new results.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
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A finite element model of the Z-crimp shaping from a hard sheet blank is developed and a number of calculations using the
ANSYS finite element software is conducted. The calculations are carried out in the framework of elastoplastic behavior of
the blank material using the classical model of bilinear kinematic (translational) hardening with corresponding parameters
of elasticity and plasticity. The model takes into account kinematics of spatial transformation of the shaping equipment as
well as the time-variable conditions of its contact interaction with the blank. 相似文献
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《Aerospace and Electronic Systems Magazine, IEEE》1994,9(2):3-8
The following topics are dealt: career development definition; career development as a part of effective management; job satisfaction issues; motivated abilities; a case study results; identification of motivational patterns; and 'reinvention' of career development 相似文献
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The paper by Koc and Chen (1994) includes new formulas for computational complexity, but the method itself is already known and has dubious numerical stability. A poorly conditioned example is shown 相似文献
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L. I. Parfenova I. M. Zakirov A. A. Konopleva A. A. Knyazev Yu. G. Galyametdinov 《Russian Aeronautics (Iz VUZ)》2011,54(1):95-98
The techniques of injecting nanomodifiers into the sulphamate electrolyte used for electrolytic forming of nickel antiabrasive
protective tipping are considered. The optimal concentration of surfactant and nanomodifier are determined. The graphs are
also presented. 相似文献
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《Aerospace and Electronic Systems Magazine, IEEE》2000,15(9):43-45
Cars powered by fuel cells have been built and tested; however, the aerospace fuel cells could not deliver high power quickly when the driver wanted to accelerate his car. Today's hybrid electric cars carry a battery that supplies the acceleration power, and the prime power source, whether an engine or fuel cell, is not stressed with sudden load peaks. Zero air pollution becomes attainable when fuel-cells supply the prime power on a hybrid vehicle 相似文献
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F. Bagenal A. Adriani F. Allegrini S. J. Bolton B. Bonfond E. J. Bunce J. E. P. Connerney S. W. H. Cowley R. W. Ebert G. R. Gladstone C. J. Hansen W. S. Kurth S. M. Levin B. H. Mauk D. J. McComas C. P. Paranicas D. Santos-Costa R. M. Thorne P. Valek J. H. Waite P. Zarka 《Space Science Reviews》2017,213(1-4):219-287
In July 2016, NASA’s Juno mission becomes the first spacecraft to enter polar orbit of Jupiter and venture deep into unexplored polar territories of the magnetosphere. Focusing on these polar regions, we review current understanding of the structure and dynamics of the magnetosphere and summarize the outstanding issues. The Juno mission profile involves (a) a several-week approach from the dawn side of Jupiter’s magnetosphere, with an orbit-insertion maneuver on July 6, 2016; (b) a 107-day capture orbit, also on the dawn flank; and (c) a series of thirty 11-day science orbits with the spacecraft flying over Jupiter’s poles and ducking under the radiation belts. We show how Juno’s view of the magnetosphere evolves over the year of science orbits. The Juno spacecraft carries a range of instruments that take particles and fields measurements, remote sensing observations of auroral emissions at UV, visible, IR and radio wavelengths, and detect microwave emission from Jupiter’s radiation belts. We summarize how these Juno measurements address issues of auroral processes, microphysical plasma physics, ionosphere-magnetosphere and satellite-magnetosphere coupling, sources and sinks of plasma, the radiation belts, and the dynamics of the outer magnetosphere. To reach Jupiter, the Juno spacecraft passed close to the Earth on October 9, 2013, gaining the necessary energy to get to Jupiter. The Earth flyby provided an opportunity to test Juno’s instrumentation as well as take scientific data in the terrestrial magnetosphere, in conjunction with ground-based and Earth-orbiting assets. 相似文献
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The InSight mission launches in 2018 to characterize several geophysical quantities on Mars, including the heat flow from the planetary interior. This quantity will be calculated by utilizing measurements of the thermal conductivity and the thermal gradient down to 5 meters below the Martian surface. One of the components of InSight is the Mole, which hammers into the Martian regolith to facilitate these thermal property measurements. In this paper, we experimentally investigated the effect of the Mole’s penetrating action on regolith compaction and mechanical properties. Quasi-static and dynamic experiments were run with a 2D model of the 3D cylindrical mole. Force resistance data was captured with load cells. Deformation information was captured in images and analyzed using Digitial Image Correlation (DIC). Additionally, we used existing approximations of Martian regolith thermal conductivity to estimate the change in the surrounding granular material’s thermal conductivity due to the Mole’s penetration. We found that the Mole has the potential to cause a high degree of densification, especially if the initial granular material is relatively loose. The effect on the thermal conductivity from this densification was found to be relatively small in first-order calculations though more complete thermal models incorporating this densification should be a subject of further investigation. The results obtained provide an initial estimate of the Mole’s impact on Martian regolith thermal properties. 相似文献