• 천문학회보
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• 제37권2호
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• pp.107.1-107.1
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• 2012

We present the results of far-ultraviolet (FUV) observations of comet C/2001 Q4 (NEAT) obtained with Far-ultraviolet Imaging Spectrograph (FIMS) on board the Korean microsatellite STSAT-1, which operated at an altitude of 700 km in a sun-synchronous orbit. FIMS is a dual-channel imaging spectrograph (S channel 900-1150 ${\AA}$, L channel 1350-1750 ${\AA}$, ${\lambda}/{\Delta}{\lambda}$ ~ 550) with large image fields of view (S: $4^{\circ}.0{\times}4^{\prime}.6$, L: $7^{\circ}.5{\times}4^{\prime}.3$, angular resolution 5'-10') optimized for the observation of diffuse emission of astrophysical radiation. Comet C/2001 Q4 (NEAT) was observed with a scanning survey mode when it was located around the perihelion between 8 and 15 May 2004. Several important emission lines were detected including S I (1425, 1474 ${\AA}$), C I (1561, 1657 ${\AA}$) and several emission lines of CO $A^1{\Pi}-X^1{\Sigma}^+$ system in the L channel. Production rates of the notable molecules, such as C I, S I and CO, were estimated from the photon fluxes of these spectral lines and compared with previous observations. We compare the flux and the production rates in the radius of $3{\times}10^5$ km with $20{\times}10^5$ km from the central coma. We obtained L-channel image which have map size $5^{\circ}{\times}5^{\circ}$ The image was constructed for the wavelength band of L-channel (1350 - 1710 ${\AA}$. We also present the radial profiles of S I, C I, CO obtained from the spectral images of the central coma. The radial profiles of $2{\times}10^6$ km region are compared with the Haser model.

• 한국전자파학회논문지
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• 제17권11호
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• pp.1082-1088
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• 2006

과학기술위성 2호에 사용하기 위한 TT&C용 안테나로 기생 모노폴(parasitic monopole)을 사용한 Turnstile 안테나를 개발하였다. 설계된 안테나는 보우-타이 다이폴(bow-tie dipole)과 기생 모노폴의 두 복사 구조로 구성된다. 안테나의 주 복사 소자는 보우-타이 구조를 이용한 보우-타이 다이폴이며, 안테나의 대역폭을 향상시키고 안테나의 크기를 줄이는 역할을 한다 또한 기생 모노폴은 안테나의 빔 폭과 축비를 향상시키는 역할을 한다. 설계된 안테나는 특별한 정합 회로 없이 50옴의 안테나 임피던스를 가지며 과학기술위성 2호에서 사용되는 주파수 $2.075{\sim}2.282GHz$ 내에서 $140^{\circ}$ 이상의 빔 폭과 3 dB 이하의 축비 그리고 1.5 이하의 VSWR 값을 가진다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2011년도 한국우주과학회보 제20권1호
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• pp.20.1-20.1
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• 2011

We present the results of far-ultraviolet (FUV) observations of comet C/2001 Q4 (NEAT) obtained with Far-ultraviolet Imaging Spectrograph (FIMS) on board the Korean microsatellite STSAT-1, which operated at an altitude of 700 km in a sun-synchronous orbit. FIMS is a dual-channel imaging spectrograph (S channel 900-1150 ${\AA}$, L channel 1350-1750 ${\AA}$, ${\lambda}/{\Box}{\lambda}$ ~ 550) with large image fields of view (S: $4^{\circ}.0{\times}4'.6$, L: $7^{\circ}.5{\times}4'.3$, angular resolution 5'-10') optimized for the observation of diffuse emission of astrophysical radiation. Comet C/2001 Q4 (NEAT) was observed with a scanning survey mode when it was located around the perihelion between 8 and 15 May 2004. Several important emission lines were detected including S I (1425, 1474 ${\AA}$), C I (1561, 1657 ${\AA}$) and several emission lines of CO $A1{\cap}-X1{\sum}+$ system in the L channel. We estimated QCO = ($2.58\;{\pm}\;0.64)\;{\times}\;1028$ s-1 from the production rate of CO 1510 ${\AA}$. We obtained L-channel image which have map size of $5^{\circ}{\times}5^{\circ}$. The image was constructed for the wavelength band of L-channel (1350-1750 ${\AA}$).We also obtained radial profile of S I, C I, CO with line fitting from central coma.

• 항공우주산업기술동향
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• 제6권1호
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• pp.3-13
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• 2008

우주분야에서의 2007년은 역사적으로 기념할 만한 해였다. 구소련의 스푸트니크가 1957년 10월 4일 발사되어 50주년을 맞이하였고, UN이 우주의 평화적 이용을 선언한지 40주년이 되는 해이기도 하다. 그리고 2007년과 2008년 초에는 일본과 중국의 달 탐사위성 발사 성공, 유럽과 일본의 국제우주정거장 실험모듈 조립성공, 중국의 위성요격시험 시도, 그리고 한국 최초의 우주인 배출사업 성공 등 다양한 변화들이 돋보인 한 해였다. 2007년 주요국 정부의 우주개발 예산은 총 783억불로 전년 대비 36% 증가하였으며, 탐사분야에서는 세계 탐사 전략과 협력 프레임워크가 발표되면서 달탐사에 대한 전 세계 14개국의 국제협력 방향이 마련되었다. 우주산업 매출은 2006년 1,061억불 규모로 전년 대비 20% 증가하였으며, 2007년 매출은 1,739억불로 예상되고 있다. 본 논문에서는 특히 지구관측위성 연구개발과 제도, 이로 인해 파생되는 영상데이터 및 서비스 시장의 동향과 전망을 자세히 분석하였다. 우리나라의 2008년 우주개발 예산은 3,164억원이며, 2007년 우주산업 생산규모는 1억불이다. 다목적실용위성 3, 3A, 5호, 통신해양기상위성의 개발과 소형위성발사체 개발 등의 연구사업이 진행 중이며, 올 해 완공되는 나로 우주센터에서 과학기술위성2호가 탑재된 소형위성발사체를 연내 발사할 예정이다.

• 천문학논총
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• 제24권1호
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• pp.53-64
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• 2009

MIRIS is the main payload of the STSAT-3 (Science and Technology Satellite 3) and the first infrared space telescope for astronomical observation in Korea. MIRIS space observation camera (SOC) covers the observation wavelength from $0.9{\mu}m$ to $2.0{\mu}m$ with a wide field of view $3.67^{\circ}\times3.67^{\circ}$. The PICNIC HgCdTe detector in a cold box is cooled down below 100K by a micro Stirling cooler of which cooling capacity is 220mW at 77K. MIRIS SOC adopts passive cooling technique to chill the telescope below 200 K by pointing to the deep space (3K). The cooling mechanism employs a radiator, a Winston cone baffle, a thermal shield, MLI (Multi Layer Insulation) of 30 layers, and GFRP (Glass Fiber Reinforced Plastic) pipe support in the system. Optomechanical analysis was made in order to estimate and compensate possible stresses from the thermal contraction of mounting parts at cryogenic temperatures. Finite Element Analysis (FEA) of mechanical structure was also conducted to ensure safety and stability in launching environments and in orbit. MIRIS SOC will mainly perform Galactic plane survey with narrow band filters (Pa $\alpha$ and Pa $\alpha$ continuum) and CIB (Cosmic Infrared Background) observation with wide band filters (I and H) driven by a cryogenic stepping motor.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.27.1-27.1
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• 2008

KASI (Korea Astronomy and Space Science Institute) is developing a compact wide-field survey space telescope system, MIRIS (The Multi-purpose IR Imaging System) to be launched in 2010 as the main payload of the Korea Science and Technology Satellite 3. Through recent System Design Review (SDR) and Preliminary Design Review (PDR), most of the system design concept was reviewed and confirmed. The near IR imaging system adopted short F/2 optics for wide field low resolution observation at wavelength band 0.9~2.0 um minimizing the effect of attitude control system. The mechanical system is composed of a cover, baffle, optics, and detector system using a $256\times256$ Teledyne PICNIC FPA providing a $3.67\times3.67$ degree field of view with a pixel scale of 51.6 arcsec. We designed a support system to minimize heat transfer with Muti-Layer Insulation. The electronics of the MIRIS system is composed of 7 boards including DSP, control, SCIF. Particular attention is being paid to develop mission operation scenario for space observation to minimize IR background radiation from the Earth and Sun. The scientific purpose of MIRIS is to survey the Galactic plane in the emission line of Pa$\alpha$ ($1.88{\mu}m$) and to detect the cosmic infrared background (CIB) radiation. The CIB is being suspected to be originated from the first generation stars of the Universe and we will test this hypothesis by comparing the fluctuations in I (0.9~1.2 um) and H (1.2~2.0 um) bands to search the red shifted Lyman cutoff signature.

• 천문학회보
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• 제36권1호
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• pp.42.1-42.1
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• 2011

The main payload of the Science and Technology Satellite 3 (STSAT-3), Multipurpose Infrared Imaging System (MIRIS), will be equipped with the wide-field near-infrared camera. Its wide field-of-view ($3.67^{\circ}{\times}3.67^{\circ}$) is optimal for the observation of the zodiacal light (ZL), the sunlight scattered by the interplanetary dust (IPD). The MIRIS will continuously monitor the seasonal variation of the ZL towards both north and south ecliptic poles, which is caused by the asymmetries of the IPD distribution with respect to the Sun and the ecliptic plane. In addition to the monitoring observations, we are planning pointed observations for compelling structures in the ZL, the asteroidal dust bands and the gegenschein. This presentation proposes the zodiacal light observations with the MIRIS and discusses the expected results.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2010년도 한국우주과학회보 제19권1호
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• pp.26.4-27
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• 2010

The main payload of STSAT-3 (Science and Technology Satellite 3), MIRIS (Multipurpose InfraRed Imaging System) is the first Korean infrared space mission to explore the near-infrared sky with a small astronomical instrument, which is being developed by KASI. The 8-cm passively cooled telescope with a wide field of view (3.67 deg. $\times$ 3.67 deg.) will be operated in the wavelength range from 0.9 to $2{\mu}m$. It will carry out wide field imaging and the emission line survey. The main purposes of MIRIS are to perform the Cosmic Infrared Background (CIB) observation at two wide spectral bands (I and H band) and to survey the Galactic plane at $1.88{\mu}m$ wavelength, the Paschen-$\alpha$ emission line. CIB observation enables us to reveal the nature of degreescale CIB fluctuation detected by the IRTS (Infrared Telescope in Space) mission and to measure the absolute CIB level. The Pashen-$\alpha$ emission line survey of Galactic plane helps us to understand the origin of Warm Ionized Medium (WIM) and to find the physical properties of interstellar turbulence related to star formation. Here, we also discuss the observation plan with MIRIS.

• 천문학회보
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• 제39권1호
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• pp.68.1-68.1
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• 2014

We present the results of far-ultraviolet (FUV) observations of comet C/2001 Q4 (NEAT) obtained with Far-ultraviolet Imaging Spectrograph (FIMS) on board the Korean microsatellite STSAT-1, which operated at an altitude of 700 km in a sun-synchronous orbit. FIMS is a dual channel imaging spectrograph (S-channel 900-1150 ${\AA}$, L-channel 1350-1710 ${\AA}$, and ${\lambda}/{\Delta}{\lambda}$ ~ 550 for both channels) with large image fields of view (S-channel $4.0^{\circ}{\times}4.6^{\prime}$, L-channel $7.5^{\circ}{\times}4.3^{\prime}$, and angular resolution ~ $5-10^{\prime}$) optimized for the observation of diffuse emission of astrophysical radiation. Comet C/2001 Q4 (NEAT) were made in two campaigns during its perihelion approach between May 8 and 15, 2004. Based on the scanning mode observations in the wavelength band of 1400-1700 ${\AA}$, we have constructed an image of the comet with an angular size of $5^{\circ}{\times}5^{\circ}$, which corresponds to the central coma region. Several important fluorescence emission lines were detected including S I multiplets at 1429 and 1479 ${\AA}$, C I multiplets at 1561 and 1657 ${\AA}$, and the CO $A^1{\Pi}-X^1{\Sigma}^+$ Fourth Positive system; we have estimated the production rates of the corresponding species from the fluxes of these emission lines. The estimated production rate of CO was $Q_{CO}=(2.65{\pm}0.63){\times}10^{28}s^{-1}$, which is 6.2-7.4% of the water production rate and is consistent with earlier predictions. The average carbon production rate was estimated to be $Q_C={\sim}1.59{\times}10^{28}s^{-1}$, which is ~60% of the CO production rate. However, the observed carbon profile was steeper than that predicted using the two-component Haser model in the inner coma region, while it was consistent with the model in the outer region. The average sulfur production rate was $Q_S=(4.03{\pm}1.03){\times}10^{27}s^{-1}$, which corresponds to ~1% of the water production rate.

• 항공우주정책ㆍ법학회지
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• 제24권2호
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• pp.163-186
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• 2009

한국에서의 미사일 개발은 미국이 안보를 제공하는 대가로 그 개발을 180 km로 한정되어왔고 같은 맥락에서 남.북한간의 긴장이 가져올 수 있는 또 하나의 전쟁 위험성을 사전 차단하기 위한 목적으로 한국의 핵무기 개발도 취소된 바 있다. 이러한 제한은 한국이 2001년 MTCR (미사일 기술 통제 체제)에 가입하면서 미사일 개발 허용 거리가 300 km로 연장되었지만 북한이 핵무기는 물론 대포동 1,2호 발사로 5,500 km 이상의 대륙간 탄도탄미사일에 이용되는 로켓 발사를 추진하면서 제한 없는 군비 발전을 진행하는 것과 대비된다. 한국이 최근 우주 산업 개발을 본격 진흥하면서 지구 저 궤도에 인공위성을 진입시키는 것에서 장래 지상 36,000 km의 지구 정지궤도에 위성 진입을 계획하는 것을 염두에 둘 때 이러한 제한은 언제인가 해소되어야 할 것이다. 한국의 우주 산업은 대개가 그러하듯이 소형 위성 제작과 이를 타국 발사체에 의뢰하여 발사, 그리고 우리의 발사체 개발이라는 3단계로 진행되고 있다. 이미 지나간 소형과학위성의 3차에 걸친 발사에 이어 현재 5개의 위성사업이 진행되고 있는 바, 이들은 다음과 같다: - 무궁화 위성 - 과학기술위성 - 다목적 실용위성 - 한별위성 - 통신해양기상위성 2008년 이소연 우주 비행사의 탄생으로 한국민들의 우주에 관한 관심이 제고되고 있는 가운데 2009년 8월 나로 1호 발사는 실패로 끝났지만 계속 추진하여야 할 우주 산업에 있어서 하나의 거쳐야 할 과정에 불과하다. 한국의 우주 관련 국내법은 1987년 제정된 항공우주산업개발촉진법, 2005년 제정된 우주개발진흥법, 2008년 제정된 우주손해배상법이 있으나 전자 2개의 법은 소관부서가 상이한 것에 연유하여 중복되어 있고, 일부 미비한 점이 있어 개선이 요망된다.