Near-infrared imaging spectrometer onboard NEXTSat-1

被引:0
|
作者
Jeong, Woong-Seob [1 ,2 ]
Park, Sung-Joon [1 ]
Moon, Bongkon [1 ]
Lee, Dae-Hee [1 ]
Pyo, Jeonghyun [1 ]
Park, Won-Kee [1 ]
Park, Youngsik [1 ]
Kim, Il-Joong [1 ]
Ko, Kyeongyeon [1 ,2 ]
Lee, Dukhang [1 ,2 ]
Kim, Min Gyu [1 ,3 ]
Kim, Minjin [1 ,2 ]
Ko, Jongwan [1 ,2 ]
Shin, Goo-Hwan [4 ]
Chae, Jangsoo [4 ]
Matsumoto, Toshio [1 ,5 ]
机构
[1] Korea Astron & Space Sci Inst, 776 Daedeok Daero, Daejeon 34055, South Korea
[2] Korea Univ Sci & Technol, 217 Gajeong Ro, Daejeon 34113, South Korea
[3] Seoul Natl Univ, 1 Gwanak Ro, Seoul 08826, South Korea
[4] Korea Adv Inst Sci & Technol, Satellite Technol & Res Ctr, 291 Daehak Ro, Daejeon 34141, South Korea
[5] JAXA, Inst Space Astronaut Sci, Sagamihara, Kanagawa 2520206, Japan
来源
SPACE TELESCOPES AND INSTRUMENTATION 2016: OPTICAL, INFRARED, AND MILLIMETER WAVE | 2016年 / 9904卷
关键词
Star formation; Near-infrared instrument; Imaging spectrometer; Space payload; Small satellite;
D O I
10.1117/12.2232924
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared instrument optimized to the first next generation of small satellite (NEXTSat-1) in Korea. The spectro-photometric capability in the near-infrared range is a unique function of the NISS. The major scientific mission is to study the cosmic star formation history in local and distant universe. For those purposes, the NISS will perform the large areal imaging spectroscopic survey for astronomical objects and low background regions. We have paid careful attention to reduce the volume and to increase the total throughput. The newly implemented off-axis optics has a wide field of view (2 degrees x 2 degrees) and a wide wavelength range from 0.9 to 3.8 mu m. The mechanical structure is designed to consider launching conditions and passive cooling of the telescope. The compact dewar after relay-lens module is to operate the infrared detector and spectral filters at 80K stage. The independent integration of relay-lens part and primary-secondary mirror assembly alleviates the complex alignment process. We confirmed that the telescope and the infrared sensor can be cooled down to around 200K and 80K, respectively. The engineering qualification model of the NISS was tested in the space environment including the launch-induced vibration and shock. The NISS will be expected to demonstrate core technologies related to the development of the future infrared space telescope in Korea.
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页数:7
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