The Visible Telescope onboard the Chinese-French SVOM satellite

Xuewu Fan; Gangyi Zou; Jianyan Wei; Yulei Qiu; Wei Gao; Wei Wang; Wengang Yang; Jian Zhang; Chuang Li; Hui Zhao; Lijun Dan; Zongxi Song; Liangjie Feng; Guorui Ren; Chao Huang; Hao Yuan; Zhonghan Sun; Fengtao Wang; Chenjie Wang; Wei Li; Chao Shen; Ning Qi; Yue Pan

doi:10.1117/12.2561854

13 December 2020 The Visible Telescope onboard the Chinese-French SVOM satellite

Xuewu Fan, Gangyi Zou, Jianyan Wei, Yulei Qiu, Wei Gao, Wei Wang, Wengang Yang, Jian Zhang, Chuang Li, Hui Zhao, Lijun Dan, Zongxi Song, Liangjie Feng, Guorui Ren, Chao Huang, Hao Yuan, Zhonghan Sun, Fengtao Wang, Chenjie Wang, Wei Li, Chao Shen, Ning Qi, Yue Pan

Author Affiliations +

Proceedings Volume 11443, Space Telescopes and Instrumentation 2020: Optical, Infrared, and Millimeter Wave; 114430Q (2020) https://doi.org/10.1117/12.2561854
Event: SPIE Astronomical Telescopes + Instrumentation, 2020, Online Only

Abstract

The Space-based multi-band astronomical Variable Objects Monitor (SVOM) project is a dedicated satellite developed at the cooperation of China and France, aim to make prompt multi-band observations of Gamma-Ray Bursts (GRBs), the afterglows and other high-energy transient astronomical events. The Visible Telescope (VT) is one of the four payloads onboard the SVOM. VT is designed to observe the afterglows of GRBs both in the visible and near infrared bands simultaneously. The telescope can reach a limiting magnitude of +22.5Mv and provide the redshift indicators for high-Z (z<4) GRBs. VT is also designed to measure the Relative Performance Errors (RPEs) for the satellite attitude and orbit control system (AOCS), aiming to improve the pointing stability of the platform during observation. VT adopts a Ritchey-Chrétien (RC) catadioptric optical configuration with a 440mm aperture and uses the dichroic prism before the focal plane to split the incident light into blue (visible) and red (near infrared) band. Two Fine Guidance Sensor (FGS) CCDs are mounted beside the main CCD on the blue band focal plane of VT and provide sub-arcsecond pixel resolution. Fiber reinforced plastic (CFRP) composites is selected as the material of VT’s main structure to ensure enough stiffness and strength during launch. The electrical video processing circuit is carefully designed to make the readout noise below 6e-/pix (rms) in 100s exposure time. Active and passive thermal control are used together to ensure the optical performance and thermoelectric cooler (TEC) is adopted to control the main CCDs working temperature below -65°C to reduce the noise. This paper provides a comprehensive overview of the scientific requirements and the key instrument design aspects of optics, main structure, electrics, thermal control, performance test and validation results of VT.

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Xuewu Fan, Gangyi Zou, Jianyan Wei, Yulei Qiu, Wei Gao, Wei Wang, Wengang Yang, Jian Zhang, Chuang Li, Hui Zhao, Lijun Dan, Zongxi Song, Liangjie Feng, Guorui Ren, Chao Huang, Hao Yuan, Zhonghan Sun, Fengtao Wang, Chenjie Wang, Wei Li, Chao Shen, Ning Qi, and Yue Pan "The Visible Telescope onboard the Chinese-French SVOM satellite", Proc. SPIE 11443, Space Telescopes and Instrumentation 2020: Optical, Infrared, and Millimeter Wave, 114430Q (13 December 2020); https://doi.org/10.1117/12.2561854

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