星云气体的光谱研究(SING):一个专门用于研究扩展物体的紫外光谱仪

B. Chandra, B. Nair, A. Suresh, C. S. Prabha, J. Mathew, Nirmal K., Mayuresh Sarpotdar, R. Mohan, M. Safonova, S. Sriram, Jayant Murthy
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引用次数: 0

摘要

SING是一种近紫外(NUV)光谱仪,尺寸接近6U立方体卫星的形状因子。光谱仪的工作波长范围从1800 Å到3000 Å,中心波长的光谱分辨率为2 Å。摄谱仪打算在低地球轨道(LEO)上运行,其主要目标是生成仪器视场(FOV)内覆盖的天空区域的光谱图,受航天器轨道倾角的限制。有效载荷包括将光聚焦在狭缝上的卡塞格伦结构的望远镜、校正透镜、凹光栅、探测器和其他所需的电子元件。由于紫外中的事件率较低,摄谱仪采用了具有低噪声性能的光子计数检测器。该负载使用FPGA作为主要系统控制器来处理探测器读出、数据压缩和存储、健康监测和遥测。在这项工作中,我们提出了光学设计及其分析,并简要描述了有效载荷的电子子系统的体系结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Spectroscopic Investigation of Nebular Gas (SING): a dedicated NUV spectrograph to study extended objects
SING is a near ultraviolet (NUV) spectrograph with a size close to 6U CubeSat form-factor. The spectrograph operates in the wavelength range from 1800 Å to 3000 Å, with a spectral resolution of 2 Å at the central wavelength. The spectrograph is intended to operate in low Earth orbit (LEO), with the primary goal to generate spectral maps of the regions of the sky covered within the field of view (FOV) of the instrument, constrained by the orbital inclination of the spacecraft. The payload consists of the telescope in Cassegrain configuration focusing the light on the slit, the corrector lens, the concave grating, the detector, and other required electronics components. As the event rate in the UV is low, the spectrograph employs a photon-counting detector because of its low noise performance. The payload uses FPGA as the main system controller to handle the detector readout, data compression and storage, health monitoring, and telemetry. In this work, we present the optical design and its analysis, along with a brief description of the architecture of electronic subsystems of the payload.
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