• Journal of Astronomy and Space Sciences
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• 제22권3호
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• pp.187-196
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• 2005

Wanders et at.(1997)이 1996년 6월 11일부터 7월 29일까지 IUE 위 성 을 통해 얻은 NGC 7469 관측 자료를 사용하여, Feibelman & Aller(1987)가 제안한 방법으로 Si III] 1892 와 C III] 1909의 플럭스 비를 통해 전자 밀도 변화를 구하였다. STARLINK/DIPSO를 이용해 두선의 윤곽을 분리하고, Si III]에 대해 $12.4\%,$ C III]에 대해 $6.6\%$ 이내의 측정오차로 플럭스를 구할 수 있었다. 계산된 밀도(log Ne)는 최소 9.69, 최대 10.93, 평균 $10.51{\pm}0.15,$ 최대-최소 차이는 1.24를 보였다. 즉 50여일 정도의 관측기간 동안에도 밀도는 최대 17.3배 정도의 밀도 변화가 있었다. 또한, UV $continuum(1315{\AA})$에 대한 각 방출선의 지연시간은 C IV는 2일, C III}는 4일, Si III]는 8일의 지연시간을 보여, 각각 중심으로부터 0.002pc, 0.004pc, 0.006pc 떨어진 곳에서 방출선영역이 형성되고 있음을 알 수 있었다. 이러한 BLR크기와 방출선 들의 선폭으로부터 구한 운동학적 자료로부터 추정한 중심 블랙홀의 질량은 약 $10^6M_{\odot}$이다.

• 천문학논총
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• 제30권1호
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• pp.11-16
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• 2015

First light galaxies have predictable linear clustering, and are expected to produce fluctuations with a characteristic spatial power spectrum, which peaks at an angular scale of ~ 10 arcminutes and in the $1-2{\mu}m$ spectral regions. The Cosmic Infrared Background ExpeRiment 2 (CIBER2) is a dedicated sounding rocket mission for measuring the fluctuations in the extragalactic infrared background light, following up the previous successful measurements of CIBER1. With a 28.5 cm telescope accompanied with three arms of camera barrels and a dual broadband filter on each H2RG (${\lambda}_c=2.5{\mu}m$) array, CIBER2 can measure 6 bands of wide field ($1.1{\times}2.2$ degrees) up to 3 AB magnitudes deeper than CIBER1. This project is leaded by California Institute of Technology/Jet Propulsion Laboratory, collaborating internationally with Institute of Space and Astronautical Science in Japan, Korea Astronomy and Space Science Institute, Korea Basic Science Institute, and Seoul National University. The Korean team is in charge of 1) one H2RG scientific array, 2) ground station hardware and software, 3) telescope lenses, and 4) flight and test bed electronics fabrication. In this paper, we describe the detailed activities of the Korean participation as well as the current status of the CIBER2 project.

• 천문학회보
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• 제39권2호
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• pp.102-102
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• 2014

The NISS (Near-infrared Imaging Spectrometer for Star formation history) onboard NEXTSat-1 is the near-infrared instrument onboard NEXTSat-1 which is being developed by KASI. The main scientific targets are nearby galaxies, galaxy clusters, star-forming regions and low background regions in order to study the cosmic star formation history in local and distant universe. After the Preliminary Design Review, we have fixed major specifications of the NISS. The off-axis optical design with 15cm apertureis optimized to obtain a wide field of view ($2deg.{\times}2deg.$), while minimizing the sensitivity loss. The opto-mechanical structure of the NISS was designed to be safe enough to endure in the launching condition as well as the space environment. The tolerance analysis was performed to cover the wide wavelength range from 0.95 to $3.8{\mu}m$ and to reduce the degradation of optical performance due to thermal variation at the target temperature, 200K. The $1k{\times}1k$ infrared sensor is operated in the dewar at 80K stage. We confirmed that the NISS can be cooled down to below 200K in the nominal orbit through a radiative cooling. Here, we report the preliminary design of the NISS.

• 천문학회보
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• 제41권2호
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• pp.64.3-65
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• 2016

The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared instrument optimized to the Next Generation of small satellite series (NEXTSat). The capability of both imaging and low spectral resolution spectroscopy 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 main observational targets are nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optical design is optimized to have a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $3.8{\mu}m$. Two linear variable filters are used to realize the imaging spectroscopy with the spectral resolution of ~20. The mechanical structure is considered to endure the launching condition as well as the space environment. The compact dewar is confirmed to operate the infrared detector as well as filters at 80K stage. The electronics is tested to obtain and process the signal from infrared sensor and to communicate with the satellite. After the test and calibration of the engineering qualification model (EQM), the flight model of the NSS is assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. Here, we report the test results of the flight model of the NISS.

• 한국지구과학회지
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• 제28권4호
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• pp.393-404
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• 2007

본 연구의 목적은 우리나라 10학년 과학 교과서 지구 분야에 등장하는 과학적 모델을 분류해 보는 것이었다. 과학적 모델을 표상 매체, 표상 방법, 모델의 가동성이라는 세 가지 차원에서 검토할 수 있도록 개발된 분류틀을 이용하여 11종 교과서의 지구과학 관련 단원을 분석하였다. 연구의 결과, 과학 교과서들은 지구과학의 세부 영역의 본성이 반영된 영역-특이적인 모델들을 수록하고 있는 것을 알 수 있었다. 즉, '지구의 변동' 단원은 접근이 용이하지 않은 지구의 내부 구조나 판들의 운동을 표상하는 모상 모델을 많이 포함하고 있었는데, 이들은 대부분 평면적 그림 모델과 정적 모델에 속하였다. '대기와 해양' 단원에서는 일기도나 해수의 온도와 염분을 나타낸 등치선도 등을 포함한 기호모델과 도해적 모델이 많이 등장하였다. '태양계와 은하' 단원에서는 규모가 큰 천체나 그들의 운동을 표상하는 모상 모델이나 유비 모델의 비율이 상대적으로 높게 나타났다. 이러한 분석 결과가 지구과학 교육과 관련 연구에 시사하는 바를 논의하였다.

• 천문학회지
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• 제46권3호
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• pp.125-131
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• 2013

We present the relation between the genus in cosmology and the Betti numbers for excursion sets of three- and two-dimensional smooth Gaussian random fields, and numerically investigate the Betti numbers as a function of threshold level. Betti numbers are topological invariants of figures that can be used to distinguish topological spaces. In the case of the excursion sets of a three-dimensional field there are three possibly non-zero Betti numbers; ${\beta}_0$ is the number of connected regions, ${\beta}_1$ is the number of circular holes (i.e., complement of solid tori), and ${\beta}_2$ is the number of three-dimensional voids (i.e., complement of three-dimensional excursion regions). Their sum with alternating signs is the genus of the surface of excursion regions. It is found that each Betti number has a dominant contribution to the genus in a specific threshold range. ${\beta}_0$ dominates the high-threshold part of the genus curve measuring the abundance of high density regions (clusters). ${\beta}_1$ dominates the genus near the median thresholds which measures the topology of negatively curved iso-density surfaces, and ${\beta}_2$ corresponds to the low-threshold part measuring the void abundance. We average the Betti number curves (the Betti numbers as a function of the threshold level) over many realizations of Gaussian fields and find that both the amplitude and shape of the Betti number curves depend on the slope of the power spectrum n in such a way that their shape becomes broader and their amplitude drops less steeply than the genus as n decreases. This behaviour contrasts with the fact that the shape of the genus curve is fixed for all Gaussian fields regardless of the power spectrum. Even though the Gaussian Betti number curves should be calculated for each given power spectrum, we propose to use the Betti numbers for better specification of the topology of large scale structures in the universe.

• 천문학회보
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• 제42권1호
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• pp.40.1-40.1
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• 2017

The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared spectro-photometric instrument optimized to the Next Generation of small satellite series (NEXTSat). To achieve the major scientific objectives for the study of the cosmic star formation in local and distant universe, the spectro-photometric survey covering more than 100 square degree will be performed. The main observational targets will be nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optics was developed to cover a wide field of view ($2deg.{\times}2deg.$) as well as the wide wavelength range from 0.95 to $2.5{\mu}m$, which were revised based upon the recent test and evaluation of the NISS instrument. The mechanical structure were tested under the launching condition as well as the space environment. The signal processing from infrared sensor and the communication with the satellite were evaluated after the integration into the satellite. The flight model of the NSS was assembled and integrated into the satellite. To verify operations of the satellite in space, the space environment tests such as the vibration, shock and thermal-vacuum test were performed. The accurate calibration data were obtained in our test facilities. Here, we report the test results of the flight model of the NISS.

• 천문학회보
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• 제43권1호
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• pp.47.1-47.1
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• 2018

The NISS (Near-infrared Imaging Spectrometer for Star formation history) onboard NEXTSat-1 have successfully developed by KASI. The capability of both imaging and spectroscopy is a unique function of the NISS. At first, it have realized the low-resolution spectroscopy (R~20) with a wide field of view of $2{\times}2deg$. in a wide near-infrared range from 0.95 to $2.5{\mu}m$. The major scientific mission is to study the cosmic star formation history in local and distant universe. It will also demonstrate the space technologies related to the infrared spectro-photometry in space. Now, the NISS is ready to launch in late 2018. After the launch, the NISS will be operated during 2 years. As an extension of the NISS, the SPEHREx (Spectro-Photometer for the History of the Universe Epoch of Reionization, and Ices Explorer) is the NASA MIDEX (Medium-class Explorer) mission proposed together with KASI (PI Institute: Caltech). It will perform the first all-sky infrared spectro-photometric survey to probe the origin of our Universe, to explore the origin and evolution of galaxies, and to explore whether planets around other stars could harbor life. Compared to the NISS, the SPHEREx is designed to have much more wide FoV of $3.5{\times}11.3deg$. as well as wide spectral range from 0.75 to $5.0{\mu}m$. After passing the first selection process, the SPHEREx is under the Phase-A study. The final selection will be made in the end of 2018. Here, we report the status of the NISS and SPHEREx missions.

• 한국지구과학회지
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• 제30권1호
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• pp.69-80
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• 2009

본 연구에서는 SDSS DR6을 이용하여 별탄생율과 활동성 은하핵의 막대의 특성, 특히 막대의 세기에 대한 의존성을 조사하였다. 막대의 세기를 보다 잘 표현하기 위하여 막대의 길이와 축비를 이용하여 막대를 6개의 군으로 나누었다. $H{\alpha}$ 방출선 세기로부터 구한 별탄생율은 막대의 세기와 좋은 상관관계를 보였으나 활동성 은하핵은 막대와 또렷한 상관관계를 보이지 않았다. 전자의 상관관계는 막대에 의해 유발되는 가스 유입이 막대의 세기에 의존하기 때문이라고 해석되며, 활동성 은하핵이 막대의 특성과 특별한 상관관계를 보이지 않는 것은 초중량 블랙홀로 들어가는 가스의 양이 막대와 초거대 블랙홀과의 상호 작용에 의해 조절된다는 것을 의미한다. 활동성 은하핵은 주변의 밀도에 의해 영향을 받으나 별탄생율은 주변의 밀도와 무관해 보인다. 이것은 별탄생은 은하에서의 가스 밀도에 의해 결정되는 국지적인 현상인데 반해 활동성 은하핵은 질량이나 광도와 같은 은하의 특성이 밀도-광도관계로 표현되는 은하의 환경 의존성과 밀접한 관계가 있음을 암시한다.

• 천문학회지
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• 제37권4호
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• pp.199-203
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• 2004

The gas response to a proposed spiral stellar pattern for our Galaxy is presented here as calculated via 2D hydrodynamic calculations utilizing the ZEUS code in the disk plane. The locus is that found by Drimmel (2000) from emission profiles in the K band and at 240 ${\mu}m$. The self-consistency of the stellar spiral pattern was studied in previous work (see Martos et al. 2004). It is a sensitive function of the pattern rotation speed, $\Omega$p, among other parameters which include the mass in the spiral and its pitch angle. Here we further discuss the complex gaseous response found there for plausible values of $\Omega$p in our Galaxy, and argue that its value must be close to $20 km s^{-l}\;kpc^{-1}$ from the strong self-consistency criterion and other recent, independent studies which depend on such parameter. However, other values of $\Omega$p that have been used in the literature are explored to study the gas response to the stellar (K band) 2-armed pattern. For our best fit values, the gaseous response to the 2-armed pattern displayed in the K band is a four-armed pattern with complex features in the interarm regions. This response resembles the optical arms observed in the Milky Way and other galaxies with the smooth underlying two-armed pattern of the old stellar disk populations in our interpretation. The complex gaseous response appears to be related to resonances in stellar orbits. Among them, the 4:1 resonance is paramount for the axisymmetric Galactic model employed, and the set of parameters explored. In the regime seemingly proper to our Galaxy, the spiral forcing appears to be marginally strong in the sense that the 4:1 resonance terminates the stellar pattern, despite its relatively low amplitude. In current work underway, the response for low values of $\Omega$p tends to remove most of the rich structure found for the optimal self-consistent model and the gaseous pattern is ring-like. For higher values than the optimal, more features and a multi-arm structure appears.