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Sounding rocket payload designed for investigations of the distribution and dynamics of the hot component of the interstellar medium using a field-widened spatial heterodyne spectrometer

机译:探测火箭有效载荷设计用于使用现场加宽的空间外差光谱仪对星际介质的热部件的分布和动力学的研究

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We are developing a field-widened spatial heterodyne spectrometer (SHS) for suborbital observations of the hot component of the diffuse interstellar medium. Our goal for these observations is to obtain the first velocity-resolved (20 km/s) line profiles of the C IV 154.8, 5.1 nm emission line from the Cygnus loop and from one direction at high galactic latitude. Long term, our interest is to develop an SHS instrument for a radial-velocity-resolved sky survey of the 10$+5$/ K 'coronal gas' in the interstellar medium using a small satellite. This paper reviews the scientific motivation and SHS concept and then discusses in more detail the optical design of the sounding rocket payload and the data taking strategy for the observations.
机译:我们正在开发一种用于弥漫性间隙介质的副血压观察的现场加宽的空间外差光谱仪(SHS)。我们对这些观测的目标是从Cygnus环路和高银河纬度的一个方向从Cygnus Loop获得第一个速度分辨(20km / s)线轮廓。长期来看,我们的兴趣是开发SHS仪器,用于使用小型卫星在星际介质中的10美元+ 5美元/ k'冠状气体的径向速度解决的天空调查。本文审查了科学动机和SHS概念,然后更详细地讨论了探测火箭有效载荷的光学设计以及对观测的策略进行策略。

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