• Title/Summary/Keyword: instrumentation: spectrographs

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FABRY-PEROT SPECTROMETER IN ASTRONOMY (FABRY-PEROT 분광기의 특성과 천문학의 적용)

  • PAK SOOJONG
    • Publications of The Korean Astronomical Society
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    • v.15 no.spc1
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    • pp.127-132
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    • 2000
  • The purposes of spectroscopy in astronomy are to measure the radiation flux of the spectroscopic emission or absorption line and to measure the dynamical parameters of the line profile. In order to use an appropriate instrument for the scientific purpose, we need to understand the characteristics of various spectrometers, e.g., a prism spectrometer, a grating spectrometer, and a Fabry-Perot spectrometer (FPS), which are being used in ultra-violet, optical, and infrared bands. The Fabry­Perot spectrometer is not very popular compared to the grating spectrometer, because of its complex and tricky operations. The Fabry-Perot spectrometer, however, can get a two-dimensional image at one exposure, so we can study radiation mechanisms and dynamical properties of extended sources, e.g., clusters, nebula, and galaxies.

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OPTICAL DESIGN OF FIMS TYPE FAR ULTRAVIOLET SPECTROGRAPH FOR SPACE OBSERVATION (FIMS 타입의 우주관측용 원자외선분광기 광학설계)

  • SEON KWANG-IL;YUK IN-SOO;RYU KWANG-SUN;LEE DAE-HEE
    • Publications of The Korean Astronomical Society
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    • v.19 no.1
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    • pp.65-70
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    • 2004
  • An imaging spectrograph concept optimized for extended far-ultraviolet emission sources is presented. Although the design was originally developed for FIMS aboard the first Korean science satellite STSAT-l launched on September 27, 2003, no rigorous theoretical background of the spectrograph design has been published. The spectrograph design employs an off-axis parabolic cylinder mirror in front of a slit that guides lights to a diffraction grating. The concave grating provides moderate spatial resolution over a large field of view. This mapping capability is absent in most astronomical instruments but is crucial to the understanding of the nature of a variety of astrophysical phenomena. The aberration theory presented in this paper can be extended to holographic gratings in order to improve the spatial as well as the spectral resolutions.

FUV IMAGING SPECTROSCOPIC OBSERVATIONS OF INTERSTELLAR MEDIUM WITH FIMS

  • SEON KWANG-IL;HAN WONYONG;LEE DAE-HEE;NAM UK-WON;PARK JANG-HYUN;YUK IN-SOO;JIN HO;MIN KYUNG WOOK;RYU KWANG-SUN;EDELSTEIN JERRY;KORPELA ERIC
    • Journal of The Korean Astronomical Society
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    • v.38 no.2
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    • pp.69-72
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    • 2005
  • The FIMS (Far-ultraviolet IMaging Spectrograph; also known as SPEAR, Spectroscopy of Plasma Evolution from Astrophysical Radiation) is the primary payload of the STSAT-1, the first Korean science satellite, which was launched in September, 2003. The FIMS performs spectral imaging of diffuse far-ultraviolet emission with the unprecedented wide field of view and the relatively good spectral resolution. We present far-ultraviolet spectral observations of highly ionized interstellar medium including supernova remnants, superbubbles, soft X-ray shadows, and the molecular hydrogen fluorescent emission lines. The FIMS has detected He II, C III, 0 III, O IV, Si IV, O VI, and $H_2$ fluorescent emission lines. The emission lines arise in shocked or thermally heated and in photo-ionized gases. We present an overview of the FIMS instrument and its initial observational results.

IGRINS MIRROR MOUNT DESIGN FOR FIVE FLAT MIRRORS (다섯 개의 평면경을 위한 IGRINS 미러 마운트 설계)

  • Oh, Jae Sok;Park, Chan;Kim, Kang-Min;Chun, Moo-Young;Yuk, In-Soo;Oh, Heeyoung;Jeong, Ueejeong;Yu, Young Sam;Lee, Hanshin;Lee, Sungho
    • Publications of The Korean Astronomical Society
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    • v.30 no.1
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    • pp.17-29
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    • 2015
  • The IGRINS is a near infrared high resolution spectrograph jointly developed by the Korea Astronomy and Space Science Institute and the University of Texas at Austin. We present design and fabrication of the optomechanical mount for the five mirrors, i.e., an input fold mirror, a slit mirror, a dichroic, and two camera fold mirrors. Based on the structure analysis and the thermal analysis of finite element methods, the optomechanical mount scheme satisfies the mechanical and the thermal design requirements given by the optical tolerance analysis. The performance of the fabricated mirror mounts has been verified through three IGRINS commissioning runs.

CONSTRUCTION OF AN E-CALLISTO STATION IN KOREA

  • Bong, Su-Chan;Kim, Yeon-Han;Roh, Hee-Seon;Cho, Kyung-Suk;Park, Young-Deuk;Choi, Seong-Hwan;Baek, Ji-Hye;Monstein, Christian;Benz, Arnold O.;Moon, Yong-Jae;Kim, Sung-Soo S.
    • Journal of The Korean Astronomical Society
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    • v.42 no.1
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    • pp.1-7
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    • 2009
  • The e-CALLISTO is a global network of frequency-agile solar radio spectrometers that was constructed in a collaboration between Swiss Federal Institute of Technology Zurich (ETH Zurich) and local host institutes. It is intended to monitor solar radio bursts 24 hours a day in frequency range between 45 MHz and 870 MHz. One of e-CALLISTO spectrometer was installed at Korea Astronomy and Space Science Institute (KASI) in 2007 October. The spectrometer gets signals from a horizontally polarized log-periodic antenna mounted on an automatic Sun-tracking system. Tracking status and data are monitored in Space Weather Monitoring Laboratory (SWML) of KASI in real time, and flare time data are transferred to ETH Zurich data archive daily. Using this spectrometer we obtained a couple of type II solar radio bursts on 2007 December 31, and found that these bursts are associated with a CME which occurred on the east limb.

DEVELOPMENT OF AN AUTOMATIC OBSERVATION SYSTEM FOR KOREAN e-CALLISTO STATION (한국 e-CALLISTO 관측소 자동 관측 시스템 개발)

  • PARK, JONGYEOB;CHOI, SEONGHWAN;BONG, SU-CHAN;KWON, YONGJUN;BAEK, JI-HYE;JANG, BI-HO;CHO, KYUNG-SUK;MOON, YONG-JAE;Monstein, Christian
    • Publications of The Korean Astronomical Society
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    • v.30 no.3
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    • pp.811-819
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    • 2015
  • The e-CALLISTO is a network of CALLISTO (Compact Astronomical Low-frequency, Low-cost Instrument for Spectroscopy in Transportable Observatories) spectrometers which detect solar radio bursts 24 hours a day in frequency range 45-870 MHz. The number of channels per spectrum is 200 and the time resolution of whole spectrum is 0.25 second. The Korean e-CALLISTO station was developed by Korea Astronomy and Space Science Institute (KASI) collaborating with Swiss Federal Institute of Technology Zurich (ETH Zurich) since 2007. In this paper, we report replacement of the tracking mount and development of the control program using Visual C++/MFC. The program can make the tracking mount track the Sun and schedule CALLISTO to start and to finish its observation automatically using the Solar Position Algorithm (SPA). Daily tracking errors (RMSE) are 0.0028 degree in azimuthal axis and 0.0019 degree in elevational axis between 2014 January and 2015 July. We expect that the program can save time and labor to make the observations of solar activity for space weather monitoring, and improve CALLISTO data quality due to the stable and precise tracking methods.

AN EVALUATION OF THE SOLAR RADIO BURST LOCATOR (SRBL) AT OVRO

  • HwangBo, J.E.;Bong, Su-Chan;Cho, K.S.;Moon Y.J.;Lee, D.Y.;Park, Y.D.;Gary Dale E.;Dougherty Brian L.
    • Journal of The Korean Astronomical Society
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    • v.38 no.4
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    • pp.437-443
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    • 2005
  • The Solar Radio Burst Locator (SRBL) is a spectrometer that can observe solar microwave bursts over a wide band (0.1-18 GHz) as well as detect the burst locations without interferometry or mechanical scanning. Its prototype has been operated at Owens Valley Radio Observatory (OVRO) since 1998. In this study, we have evaluated the capability of the SRBL system in flux and radio burst location measurements. For this, we consider 130 microwave bursts from 2000 to 2002. The SRBL radio fluxes of 53 events were compared with the fluxes from USAF/RSTN and the burst locations of 25 events were compared with the optical flare locations. From this study, we found: (1) there is a relatively good correlation (r = 0.9) between SRBL flux and RSTN flux; (2) the mean location error is about 8.4 arcmin and the location error (4.7 arcmin) of single source events is much smaller than that (14.9 arcmin) of multiple source events; (3) the minimum location error usually occurred just after the starting time of burst, mostly within 10 seconds; (4) there is a possible anti-correlation (r = -0.4) between the pointing error of SRBL antenna and the location error. The anti-correlation becomes more evident (r=-0.9) for 6 strong single source events associated with X-class flares. Our results show that the flux measurement of SRBL is consistent with that of RSTN, and the mean location error of SRBL is estimated to be about 5 arcmin for single source events.

CONCEPTUAL STRUCTURAL DESIGN AND COMPARATIVE POWER SYSTEM ANALYSIS OF OZONE DYNAMICS INVESTIGATION NANO-SATELLITE (ODIN)

  • Park, Nuri;Hwang, Euidong;Kim, Yeonju;Park, Yeongju;Kang, Deokhun;Kim, Jonghoon;Hong, Ik-seon;Jo, Gyeongbok;Song, Hosub;Min, Kyoung Wook;Yi, Yu
    • Journal of The Korean Astronomical Society
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    • v.54 no.1
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    • pp.9-16
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    • 2021
  • The Ozone Dynamics Investigation Nano-Satellite (ODIN) is a CubeSat design proposed by Chungnam National University as contribution to the CubeSat Competition 2019 sponsored by the Korean Aerospace Research Institute (KARI). The main objectives of ODIN are (1) to observe the polar ozone column density (latitude range of 60° to 80° in both hemispheres) and (2) to investigate the chemical dynamics between stratospheric ozone and ozone depleting substances (ODSs) through spectroscopy of the terrestrial atmosphere. For the operation of ODIN, a highly efficient power system designed for the specific orbit is required. We present the conceptual structural design of ODIN and an analysis of power generation in a sun synchronous orbit (SSO) using two different configurations of 3U solar panels (a deployed model and a non-deployed model). The deployed solar panel model generates 189.7 W through one day which consists of 14 orbit cycles, while the non-deployed solar panel model generates 152.6 W. Both models generate enough power for ODIN and the calculation suggests that the deployed solar panel model can generate slightly more power than the non-deployed solar panel model in a single orbit cycle. We eventually selected the non-deployed solar panel model for our design because of its robustness against vibration during the launch sequence and the capability of stable power generation through a whole day cycle.

SOMANGNET: SMALL TELESCOPE NETWORK OF KOREA

  • Im, Myungshin;Kim, Yonggi;Lee, Chung-Uk;Lee, Hee-Won;Pak, Soojong;Shim, Hyunjin;Sung, Hyun-Il;Kang, Wonseok;Kim, Taewoo;Heo, Jeong-Eun;Hinse, Tobias C.;Ishiguro, Masateru;Lim, Gu;Ly, Cuc T.K.;Paek, Gregory S.H.;Seo, Jinguk;Yoon, Joh-na;Woo, Jong-Hak;Ahn, Hojae;Cho, Hojin;Choi, Changsu;Han, Jimin;Hwang, Sungyong;Ji, Tae-Geun;Lee, Seong-Kook J.;Lee, Sumin;Lee, Sunwoo;Kim, Changgon;Kim, Dohoon;Kim, Joonho;Kim, Sophia;Jeong, Mankeun;Park, Bomi;Paek, Insu;Kim, Dohyeong;Park, Changbom
    • Journal of The Korean Astronomical Society
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    • v.54 no.3
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    • pp.89-102
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    • 2021
  • Even in an era where 8-meter class telescopes are common, small telescopes are considered very valuable research facilities since they are available for rapid follow-up or long term monitoring observations. To maximize the usefulness of small telescopes in Korea, we established the SomangNet, a network of 0.4-1.0 m class optical telescopes operated by Korean institutions, in 2020. Here, we give an overview of the project, describing the current participating telescopes, its scientific scope and operation mode, and the prospects for future activities. SomangNet currently includes 10 telescopes that are located in Australia, USA, and Chile as well as in Korea. The operation of many of these telescopes currently relies on operators, and we plan to upgrade them for remote or robotic operation. The latest SomangNet science projects include monitoring and follow-up observational studies of galaxies, supernovae, active galactic nuclei, symbiotic stars, solar system objects, neutrino/gravitational-wave sources, and exoplanets.

Opening New Horizons with the L4 Mission: Vision and Plan

  • Kyung-Suk Cho;Junga Hwang;Jeong-Yeol Han;Seong-Hwan Choi;Sung-Hong Park;Eun-Kyung Lim;Rok-Soon Kim;Jungjoon Seough;Jong-Dae Sohn;Donguk Song;Jae-Young Kwak;Yukinaga Miyashita;Ji-Hye Baek;Jaejin Lee;Jinsung Lee;Kwangsun Ryu;Jongho Seon;Ho Jin;Sung-Jun Ye;Yong-Jae, Moon;Dae-Young Lee;Peter H. Yoon;Thiem Hoang;Veerle Sterken;Bhuwan Joshi;Chang-Han Lee;Jongjin Jang;Jae-Hwee Doh;Hwayeong Kim;Hyeon-Jeong Park;Natchimuthuk Gopalswamy;Talaat Elsayed;John Lee
    • Journal of The Korean Astronomical Society
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    • v.56 no.2
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    • pp.263-275
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    • 2023
  • The Sun-Earth Lagrange point L4 is considered as one of the unique places where the solar activity and heliospheric environment can be observed in a continuous and comprehensive manner. The L4 mission affords a clear and wide-angle view of the Sun-Earth line for the study of the Sun-Earth and Sun-Moon connections from he perspective of remote-sensing observations. In-situ measurements of the solar radiation, solar wind, and heliospheric magnetic field are critical components necessary for monitoring and forecasting the radiation environment as it relates to the issue of safe human exploration of the Moon and Mars. A dust detector on the ram side of the spacecraft allows for an unprecedented detection of local dust and its interactions with the heliosphere. The purpose of the present paper is to emphasize the importance of L4 observations as well as to outline a strategy for the planned L4 mission with remote and in-situ payloads onboard a Korean spacecraft. It is expected that the Korean L4 mission can significantly contribute to improving the space weather forecasting capability by enhancing the understanding of heliosphere through comprehensive and coordinated observations of the heliosphere at multi-points with other existing or planned L1 and L5 missions.