首页> 外文会议>Conference on X-Ray and Gamma-Ray Instrumentation for Astronomy XI 2-4 August 2000 San Diego, USA >A Sounding Rocket Mission to Study the Solar Soft X-RAY and EUV Emission using Transition-Edge Sensor Technology
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A Sounding Rocket Mission to Study the Solar Soft X-RAY and EUV Emission using Transition-Edge Sensor Technology

机译:用过渡边缘传感器技术研究太阳软X射线和EUV发射的探空火箭任务

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We are developing a new sounding rocket payload, the Advanced Technology Solar Spectroscopic Imager (ATSSI), that will use an 8 x 8 array of transition edge sensors (TES) to obtain true spectroheliograms in a spectral bandpass spanning approx 50 eV to approx 3 keV. The TES array will be flown at the focus of a Wolter I telescope, where it will image a 3 arc-min by 3 arc-min field of view with a pixel resolution of approx 6 arc-sec. In this way, it will obtain aprpox 1000 individual spectra with an expected average energy resolution of approx3 eV FWHM. In addition to the TES array, the ATSSI will employ six multilayer telescopes with bandpasses centered on atomic lines at 17.1 A (Fe XVII), 195.1 A (Fe XII), 171.1 A (Fe IX), 57.9 A (Mg X), 98.3 A (Ne VIII), and 150.1 A (O VI). Two additional telescopes with bandpasses centered at 1550 A (Fe IX), 57.9 A (Mg X), 98.3 A (Ne VIII), and 150.1 A (O VI). Two additional telescopes with bandpasses centered at 1550 A (C IV) and 1216 A (H I) will also be used. The eight narrowband telescopes will provide high spatial resolution (<= 1 arc-sec), full-disk solar images and will be complemented by two grating slit spectroheliographs. One grating will obtain high resolution spectroheliograms between 2750 A and 2850 A (for Mg II h- and k-line studies), and the other will be multilayer-based and will probe the Fe IX/X - O V/VI complex around 171 A (73 eV). With this set of instruments, we expect to explore more fully the nature of the energy flow between small-scale coronal, chromospheric and transition region structures, as well as to address the issue of what mechanisms are responsible for heating the quiescent solar atmosphere.
机译:我们正在开发一种新的探空火箭有效载荷,即先进技术太阳光谱成像仪(ATSSI),它将使用8 x 8过渡边缘传感器(TES)阵列在跨度约50 eV至约3 keV的光谱带通中获得真实的光谱图。 。 TES阵列将在Wolter I望远镜的焦点上飞行,它将以3弧分x 3弧分的视场成像,像素分辨率约为6弧秒。这样,它将获得aprpox 1000单个光谱,其预期平均能量分辨率约为3 eV FWHM。除TES阵列外,ATSSI将采用六只多层带通孔,其带通集中在原子线上,分别为17.1 A(Fe XVII),195.1 A(Fe XII),171.1 A(Fe IX),57.9 A(Mg X),98.3 A(Ne VIII)和150.1 A(O VI)。另外两台带通的望远镜分别位于1550 A(Fe IX),57.9 A(Mg X),98.3 A(Ne VIII)和150.1 A(O VI)。还将使用另外两个带通量分别为1550 A(C IV)和1216 A(H I)的望远镜。八台窄带望远镜将提供高空间分辨率(<= 1弧秒)的全盘太阳图像,并将由两个光栅狭缝光谱仪进行补充。一个光栅将获得2750 A和2850 A之间的高分辨率光谱图(用于Mg II h和k线研究),另一个光栅将是基于多层的并将探测171 A附近的Fe IX / X-OV / VI络合物。 (73 eV)。借助这套仪器,我们希望能更全面地探索小规模日冕,色球层和过渡区域结构之间的能量流性质,并解决引起静态太阳大气加热的机理问题。

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