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MIRIS 우주관측카메라의 기계부 개발 (DEVELOPMENT OF THE MECHANICAL STRUCTURE OF THE MIRIS SOC)

  • 문봉곤;정웅섭;차상목;이창희;박성준;이대희;육인수;박영식;박장현;남욱원;;;양순철;이선희;이승우;한원용
    • 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.

한국형 다단연소사이클 로켓엔진 개발 동향 (Development Trend of Korean Staged Combustion Cycle Rocket Engine)

  • 김채형;한영민;조남경;김승한;유병일;이광진;소윤석;우성필;임지혁;황창환;이정호;김진한
    • 한국추진공학회지
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    • 제22권3호
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    • pp.109-118
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    • 2018
  • 한국형발사체(KSLV-II) 개발과 함께 지구정지궤도 발사를 위해 비추력이 높은 다단연소사이클 로켓 엔진 개발이 한국항공우주연구원에서 진행되고 있다. 다단연소사이클 로켓엔진은 한국형발사체 엔진과 달리 가스발생기를 사용하는 개방형 엔진이 아니며, 크게 예연소기, 터보펌프, 주연소기로 구성되어 있는 폐쇄형 엔진이다. 기술검증시제 개발용 모델(TDM0)을 조립하여 나로우주센터의 7톤급 엔진 연소시험설비에서 연소시험이 진행되고 있으며, 기술검증시제 모델의 연소시험은 성공적으로 수행되었다.

과학기술위성3호 소형영상분광기 발사모델 환경시험 결과 (Environmental Test Results of a Flight Model of a Compact Imaging Spectrometer for a Microsatellite STSAT-3)

  • 이상준;김정현;이준호;이치원;장태성;강경인
    • 한국광학회지
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    • 제22권4호
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    • pp.184-190
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    • 2011
  • 과학기술위성3호 부탑재체인 소형영상분광기 COMIS(Compact Imaging Spectrometer)는 400 - 1050 nm의 관측 대역에서 분광 관측을 수행하는 영상 분광기이다. COMIS는 2012년 고도 700 km의 원 궤도에서 발사 된 후 27 m의 공간분해능과 2 - 15 nm의 파장 분해능을 갖도록 설계되었다. 본 논문에서는 COMIS 비행 모델의 환경시험 수행결과를 기술한다. 발사 환경인 진동 가진에 의한 영상분광기의 광학적, 구조적인 변화 여부와 우주환경인 열.진공 상태에서의 기능 시험을 수행하여 안정성 및 신뢰성을 검증 받았다. 우주공간에서의 환경으로 일컬어지는 고진공($10^{-5}$ torr이하)과 $-30^{\circ}C{\sim}35^{\circ}C$의 고온 및 저온의 열적 변화 상태를 모사하는 시험에서 정상적인 기능을 보였고, 10 grms의 랜덤 진동 가진 전.후의 고유 진동수는 1% 이내의 변화량을 보였다. 환경시험 전 후로 영상분광기의 변조전달함수(MTF, Modulation Transfer Function) 측정을 하여 광학 성능이 유지됨을 확인하였다. 환경시험을 마친 영상분광기는 현재 과학기술위성3호 본체와의 조립을 진행 중에 있으며 2012년 발사 예정에 있다.

$Ag_2CdSnSe_4$$Ag_2CdSnSe_4:Co^{+2}$단결정의 광학적 특성 (Optical properties of $Ag_2CdSnSe_4$ and $Ag_2CdSnSe_4:CO^{2+}$ single crystals)

  • 이충일
    • 한국진공학회지
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    • 제10권1호
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    • pp.16-21
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    • 2001
  • 4원 화합물 반도체인 $Ag_2CdSnSe_4$$Ag_2CdSnSe_4$:$CO^{2+}$ 단결정을 화학수송법으로 성장시켜 광학적 특성을 조사하였다. 성장된 결정들은 wurtzite 결정구조로서 격자상수는 각각 a = 4.357 $\AA$, c = 7.380 $\AA$($Ag_2CdSnSe_4$:$CO^{2+}$)이었다. 298k에서의 광 흡수 측정으로부터 구한 에너지 띠 간격은 순수한 $Ag_2$CdSnSe의 경우 1.21eV, cobalt 불순물로 첨가한 $Ag_2CdSnSe_4$의 경우 1.02ev이었으며, cobalt를 불순물로 첨가함에 따라 190meV의 에너지 띠 간격의 감소를 보였다. $Ag_2CdSnSe_4$ 결정의 광 흡수 스펙트럼에서 4개의 흡수 피크들을 관측하였으며, 이들 피크 들은 $T_d$결정장내에서 스핀 - 궤도결합효과에 의한 $Co^{2+}$ 이온의 분리된 준위사이의 전자전이에 의한 것으로 설명되었다.

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The Far-ultraviolet Spectrum Study of Comet C/2001 Q4 (NEAT)

  • Lim, Yeo-Myeong;Min, Kyoung-Wook;Feldman, Paul D.;Han, Wanyong;Edelstein, Jerry
    • 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.

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Progress Report on NISS onboard NEXTSat-1

  • Jeong, Woong-Seob;Park, Sung-Joon;Park, Kwijong;Moon, Bongkon;Lee, Dae-Hee;Pyo, Jeonghyun;Park, Youngsik;Kim, Il-Joong;Park, Won-Kee;Lee, Duk-Hang;Park, Chan;Ko, Kyeongyeon;Nam, Ukwon;Han, Wonyong;Im, Myungshin;Lee, Hyung Mok;Lee, Jeong-Eun;Shin, Goo-Hwan;Chae, Jangsoo;Matsumoto, Toshio
    • 천문학회보
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    • 제39권1호
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    • pp.49.1-49.1
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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 imaging low-resolution spectroscopic observation in the near-infrared range for nearby galaxies, low background regions, star-forming regions and so on will be performed on orbit. After the System Requirement Review, the optical design is changed from on-axis to the off-axis telescope which has a wide field of view (2 deg. ${\times}$ 2 deg.) as well as the wide wavelength range from 0.95 to $3.8{\mu}m$. The mechanical structure is considered to endure the launching condition as well as the space environment. The design of relay optics is optimized to maintain the uniform optical performance in the required wavelength range. The stray light analysis is being made to evade a light outside a field of view. The dewar is designed to operate the infrared detector at 80K stage. From the thermal analysis, we confirmed that the telescope can be cooled down to around 200K in order to reduce the large amount of thermal noise. Here, we report the current status of the NISS development.

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Kevlar wire를 이용한 링크 구동형 우주잔해 포획장치 (A Linkage Based Space Debris Capture Device Utilizing Kevlar Wires)

  • 정진원;황보현;김희경;이건희;서민석;이동윤;김병규
    • 항공우주시스템공학회지
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    • 제11권5호
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    • pp.36-41
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    • 2017
  • 위성 궤도 내 우주 잔해가 늘어남에 따라 현재 운용 중인 위성들과 폐위성과의 충돌 위험이 지속적으로 증가하는 추세이다. 위 문제를 해결하기 위해 본 연구에서는 1 자유도의 간단한 메커니즘을 사용한 포획장치를 설계하였다. 포획장치는 net가 연결된 4개의 링크군으로 구성되었다. 또한 신뢰도를 높이기 위해 4개의 링크군을 하나의 구동부에 연결하여 자유도가 1이 되도록 설계하였다. 포획장치가 청소위성(janitor위성)의 임무수행에 영향을 끼치지 않도록 위성의 옆면에 수납하였다. 최종적으로 우주 환경에서의 전개 가능성을 파악하기 위해 미세중력 환경을 모사한 수중환경에서 포획장치 전개 실험을 수행하였다. 포획장치 전개실험 중 janitor위성과의 간섭 없이 전개완료 됨을 확인함으로써 대상 위성 포획에 대한 가능성을 검증하였다.

Generation of Ionospheric Delay in Time Comparison for a Specific GEO Satellite by Using Bernese Software

  • Jeong, Kwang Seob;Lee, Young Kyu;Yang, Sung Hoon;Hwang, Sang-wook;Kim, Sanhae;Song, Kyu-Ha;Lee, Wonjin;Ko, Jae Heon
    • Journal of Positioning, Navigation, and Timing
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    • 제6권3호
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    • pp.125-133
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    • 2017
  • Time comparison is necessary for the verification and synchronization of the clock. Two-way satellite time and frequency (TWSTFT) is a method for time comparison over long distances. This method includes errors such as atmospheric effects, satellite motion, and environmental conditions. Ionospheric delay is one of the significant time comparison error in case of the carrier-phase TWSTFT (TWCP). Global Ionosphere Map (GIM) from Center for Orbit Determination in Europe (CODE) is used to compare with Bernese. Thin shell model of the ionosphere is used for the calculation of the Ionosphere Pierce Point (IPP) between stations and a GEO satellite. Korea Research Institute of Standards and Science (KRISS) and Koganei (KGNI) stations are used, and the analysis is conducted at 29 January 2017. Vertical Total Electron Content (VTEC) which is generated by Bernese at the latitude and longitude of the receiver by processing a Receiver Independent Exchange (RINEX) observation file that is generated from the receiver has demonstrated adequacy by showing similar variation trends with the CODE GIM. Bernese also has showed the capability to produce high resolution IONosphere map EXchange (IONEX) data compared to the CODE GIM. At each station IPP, VTEC difference in two stations showed absolute maximum 3.3 and 2.3 Total Electron Content Unit (TECU) in Bernese and GIM, respectively. The ionospheric delay of the TWCP has showed maximum 5.69 and 2.54 ps from Bernese and CODE GIM, respectively. Bernese could correct up to 6.29 ps in ionospheric delay rather than using CODE GIM. The peak-to-peak value of the ionospheric delay for TWCP in Bernese is about 10 ps, and this has to be eliminated to get high precision TWCP results. The $10^{-16}$ level uncertainty of atomic clock corresponds to 10 ps for 1 day averaging time, so time synchronization performance needs less than 10 ps. Current time synchronization of a satellite and ground station is about 2 ns level, but the smaller required performance, like less than 1 ns, the better. In this perspective, since the ionospheric delay could exceed over 100 ps in a long baseline different from this short baseline case, the elimination of the ionospheric delay is thought to be important for more high precision time synchronization of a satellite and ground station. This paper showed detailed method how to eliminate ionospheric delay for TWCP, and a specific case is applied by using this technique. Anyone could apply this method to establish high precision TWCP capability, and it is possible to use other software such as GIPSYOASIS and GPSTk. This TWCP could be applied in the high precision atomic clocks and used in the ground stations of the future domestic satellite navigation system.

Novel condylar repositioning method for 3D-printed models

  • Sugahara, Keisuke;Katsumi, Yoshiharu;Koyachi, Masahide;Koyama, Yu;Matsunaga, Satoru;Odaka, Kento;Abe, Shinichi;Takano, Masayuki;Katakura, Akira
    • Maxillofacial Plastic and Reconstructive Surgery
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    • 제40권
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    • pp.4.1-4.4
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    • 2018
  • Background: Along with the advances in technology of three-dimensional (3D) printer, it became a possible to make more precise patient-specific 3D model in the various fields including oral and maxillofacial surgery. When creating 3D models of the mandible and maxilla, it is easier to make a single unit with a fused temporomandibular joint, though this results in poor operability of the model. However, while models created with a separate mandible and maxilla have operability, it can be difficult to fully restore the position of the condylar after simulation. The purpose of this study is to introduce and asses the novel condylar repositioning method in 3D model preoperational simulation. Methods: Our novel condylar repositioning method is simple to apply two irregularities in 3D models. Three oral surgeons measured and evaluated one linear distance and two angles in 3D models. Results: This study included two patients who underwent sagittal split ramus osteotomy (SSRO) and two benign tumor patients who underwent segmental mandibulectomy and immediate reconstruction. For each SSRO case, the mandibular condyles were designed to be convex and the glenoid cavities were designed to be concave. For the benign tumor cases, the margins on the resection side, including the joint portions, were designed to be convex, and the resection margin was designed to be concave. The distance from the mandibular ramus to the tip of the maxillary canine, the angle created by joining the inferior edge of the orbit to the tip of the maxillary canine and the ramus, the angle created by the lines from the base of the mentum to the endpoint of the condyle, and the angle between the most lateral point of the condyle and the most medial point of the condyle were measured before and after simulations. Near-complete matches were observed for all items measured before and after model simulations of surgery in all jaw deformity and reconstruction cases. Conclusions: We demonstrated that 3D models manufactured using our method can be applied to simulations and fully restore the position of the condyle without the need for special devices.

『황제내경(黃帝內經)』에 나타난 일월성진(日月星辰)에 관(關)한 연구(硏究) (A Study on the Sun-Moon-Stars(日月星辰) appeared in Huang Ti Nei Chin(『黃帝內經』))

  • 박찬영;김기욱;박현국
    • 동국한의학연구소논문집
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    • 제5권
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    • pp.281-306
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    • 1996
  • A study on the effect of the Sun-Moon-Stars(日月星辰) in Huang Ti Nei Ching("黃帝內經") on the formation of the Yunqi theory(運氣理論) have revealed following conclusions. 1. There was a record of Stars(星辰) written by Gabgol-Character(甲骨文字) in the Yin(殷) Dynasty. But the very first documentary records of Stars(星辰) is Shu Jing("書經"). Ancient astronomy had the tendency of astrology of combined with theory of the Five Elements(五行) and finally effects the theory of formation of Huang Ti Nei Ching("黃帝內經"). 2. Shu Jing("書經") said that Junrak(錢樂) made an Armillary sphere(運天儀) in the Sung(宋) Dynasty. And in the Jin(秦) and the Han(漢) Dynasty, they already observed the stars. The Sunkiokhyung(璿機玉衡) which is machinery of star-observing, became to be called an Armillary sphere (運天儀) by the pass of times. 3. As of the theory of the Cosmos-structure(宇宙-構造論) in Ohanunhangdaeron("五運行大論"), Guiyugu(鬼兒區) announced the Hypothesis of Covering Heaven(蓋天說) but Kibak(岐伯) supported the Hypothesis of chaosheven's(蓋天說) and in the theory of atmosphere(大氣論) in Ohanunhangdaeron("五運行大論") said that the earth was in Great Empty(太虛) and it was floating in the universe by the Great Chi(大氣). 4. The knowledge about the Five stars(五星) in Huang Ti Nei Ching("黃帝內經") is presented in the section of Gemgwejineonron("金?眞言論"), Gigoupyondaeron("氣交變大論"), Youkwonjeonggidaeron("六元正紀大論").ln the method of identifying the Five stars(五星) presented the criteria of the brightness, the altitude, the colours and the orbit etc. 5. The jupiter which has twelve year's revolution cycle was the basis of determination on the Twelve constellation(12辰), the Twelve field of heaven(12次), the Twelve Houses in the ecliptic(黃道 12宮), the Twelve Earth's Branches(12支) and the Twelve fields of Earth(12分野) and also it became the origin of the duodecimals(12進法). 6. The saturn having about twenty-eight year's revolution cycle became the criterion in identifying the Twenty Eight Constellations(28宿) which was used as the coordinates of the Celestial sphere (天球). 7. By the Percussional movement(歲差運動), the position of polaris and the Vernal-Antumal equinox(春秋分点) were shifted. Therefore the ancient the Heaven Gate-Earth Door(天門-地戶) changed from the position of Sil-Byuk(室壁), Yik-Jin(翼軫). And the precisional movements brought about the concept of the WunHoyYunSe(元會運世) that is a method of dividing a period. Also the precisional movement gave three dimension(三次元) foundation interpreted the Sixty JiaZi (六十甲子) which is revolving through sixty years uniformally. 8. The Hypothesis of the Nine Houses and Eight Winds(九宮八風論) which is one field of the astrology of ancient polaris-nine Houses divination plate(太一九宮占盤) brought about the concept of deficiency and excess and the concept of the Wind Vice(風邪). In the Calendar System(曆法) presented in Huang Ti Nei Ching("黃帝內經") the tropical year of the Sun-Moon-Stars(日月星辰) and the revolution and the rotation of the earth give explanations the changes of Yin-Yang(陰陽) by the use of the ten Celestial branches(十干) and the twelve Earth branches(十二支).

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