Ground calibration of visible emission line coronagraph on board Aditya-L1 mission

IF 1.7 3区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Astronomical Telescopes Instruments and Systems Pub Date : 2023-10-17 DOI:10.1117/1.jatis.9.4.044001
Raghavendra Prasad Budihal, Venkata Suresh Narra, Natarajan Venkatasubramanyam, Pawan Kumar Somasundaram, Umesh Kamath Padavu, Shalabh Mishra, Bhavana Hegde, Sasikumar Raja Kantepalli, Jagdev Singh
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Abstract

Visible emission line coronagraph (VELC) is the prime payload on board India’s first space solar observatory Aditya-L1. VELC is a unique payload with simultaneous observational capabilities in imaging, spectroscopy, and spectro polarimetry modes. VELC is capable of achieving high spatial, spectral, and temporal resolution closer to the solar limb 1.05 R ⊙ compared to the existing space and ground-based solar coronagraphs. VELC consists of a total of 44 optical elements in 18 groups, which are custom designed and developed to meet the desired performance requirements. In addition, it consists of four mechanisms out of which two are multioperational with expected life cycle of million operations. Four detectors (three sCMOS and one InGaAs) are used to record the data. The performance of the payload depends on the performance of individual element, subsystems, and the system level performance of all the elements (such as optics, mechanism, and detectors) together. To ensure the desired performance levels are achieved, each element/subsystem should be tested prior to integrating them together. Evaluation of performance of the integrated system is essential to validate the payload capabilities to meet the proposed science goals. This paper summarizes the calibration tests carried out on the integrated system and compares the results obtained with respect to the design requirements to meet the proposed science goals.
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Aditya-L1卫星上可见光发射线日冕仪的地面标定
可见发射线日冕仪(VELC)是印度首个空间太阳天文台Aditya-L1上的主要有效载荷。VELC是一种独特的有效载荷,具有成像、光谱和光谱偏振模式的同时观测能力。与现有的空间和地面日冕仪相比,VELC能够实现接近太阳边缘1.05 R⊙的高空间、光谱和时间分辨率。VELC由18组共44个光学元件组成,这些元件是定制设计和开发的,以满足所需的性能要求。此外,它由四种机制组成,其中两种是多操作的,预期生命周期为百万次操作。四个探测器(三个sCMOS和一个InGaAs)用于记录数据。有效载荷的性能取决于单个元素、子系统的性能,以及所有元素(如光学、机制和探测器)的系统级性能。为了确保达到预期的性能水平,应该在将每个元素/子系统集成在一起之前对它们进行测试。综合系统的性能评估对于验证有效载荷能力以满足提出的科学目标至关重要。本文总结了在集成系统上进行的校准试验,并将所获得的结果与设计要求进行了比较,以满足提出的科学目标。
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来源期刊
CiteScore
4.40
自引率
13.00%
发文量
119
期刊介绍: The Journal of Astronomical Telescopes, Instruments, and Systems publishes peer-reviewed papers reporting on original research in the development, testing, and application of telescopes, instrumentation, techniques, and systems for ground- and space-based astronomy.
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