• Korean Journal of Optics and Photonics
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• v.19 no.6
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• pp.400-407
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• 2008

An Instrument to measure normal spectral emissivity is built using a Fourier Transform-Infrared (FT-IR) spectrometer. The instrument is composed of four main parts, reference blackbody, sample furnace, optics system, and FT-IR spectrometer. Measurement ranges of temperature and wavelength are $200^{\circ}C{\sim}500^{\circ}C$ and $3.5{\mu}m{\sim}20{\mu}m$, respectively. Measured emissivity of the reference blackbody is greater than 0.9993 with combined relative uncertainty less than 0.69%, which can be considered an ideal blackbody. We studied the emissivity of opaque alumina, graphite, anodized aluminum, and steel (IMS 200). It is shown that emissivity increases with the roughness of the steel (IMS 200) surface.

• Journal of the Korean earth science society
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• v.43 no.2
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• pp.312-323
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• 2022

This study began with the hypothesis of whether "solar radiation" and "terrestrial radiation" can be replaced by "visible radiation" and "infrared radiation", respectively. To this end, we investigated the perceptions of high school students who completed the Earth Science I course through a questionnaire to reveal how they perceived each concept. We also analyzed the descriptions and illustrations of textbooks that may have affected their perceptions. All of the students who participated in the questionnaire recognized solar radiation as radiation emitted only in the visible light region. About 35% of the students recognized convection, conduction, and latent heat as energy transfer by radiation in the Earth's heat budget. By analyzing six types of Earth Science I textbooks in the 2015 revised curriculum, we observed that two types introduced the terms "shortwave radiation" and "longwave radiation" but had no explanation for them, while the other two described solar radiation as "radiation mainly in the visible light region" or "radiation in short wavelengths". Regarding solar and terrestrial radiation in the last two types, there was no explanation for the wavelength regions, or ambiguous terms such as "short wavelength" and "long wavelength" were used. In addition, the two textbooks contained some errors in the illustration of the energy budget. Considering that textbooks described solar and terrestrial radiation without defining the exact terms for shortwave and longwave radiation, learners are likely to recognize solar and terrestrial radiation as visible and infrared radiation, respectively. This finding implies that vague statements or errors in textbooks can cause or reproduce students' misconceptions. The discussion in this study is expected to be used as a helpful reference material for teaching and learning processes regarding the Earth's radiation equilibrium and heat budget, and thereby contribute to proposing reasonable description plans for future textbook writing.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.49-49
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• 2010

본 논문은 진공챔버 내부에서 위성 표면의 온도를 제어하기 위한 할로겐램프를 이용한 적외선 발열장치의 개발에 관한 것으로, 인공위성이 우주궤도에서 받게 되는 복사에너지를 지상의 진공챔버 내에서 모사하기 위한 비접촉 적외선 발열장치에 관한 것이다. 진공챔버 내에서의 비접촉식 발열 방법 중, 진공환경에서의 오염을 발생시키지 않고, 발열 시간 및 냉각 시간이 가장 짧으며, 높은 열효율로 태양복사에너지를 가장 근사하게 모사할 수 있는 할로겐 램프를 이용한 발열 방법을 적용하였으며, 램프에서 방사되는 열에너지가 위성표면에 균일하게 분포될 수 있도록 위성 표면으로부터의 거리와 램프의 개수, 램프의 배열에 따른 에너지 분포 계산식을 도출하여 적용하였다. 공급 전압에 따른 램프의 저항특성을 파악하여, 원격으로 제어되는 150 VDC, 5 A의 직류전원공급기를 이용해 램프의 발열량을 조절하였으며, 발열량에 따른 위성 표면온도에 대한 해석을 수행하였다. 램프를 이용한 비접촉식 적외선 발열장치 개발을 통해 진공환경에서의 시험대상에 대한 효율적인 열에너지 부과방법 수립이 가능하였다.

• Bulletin of the Korean Space Science Society
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• 2009.10a
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• pp.25.1-25.1
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• 2009

적외선 우주배경복사 관측실험 (Cosmic Infrared Background ExpeRiment, CIBER) II는 2009년 2월 25일 화이트샌드 미사일 기지에서 NASA 사운딩 로켓에 탑재, 발사된 CIBER I의 후속 프로젝트이다. 독립적인 Imager 2 대와 Spectrometer 2 대로 구성된 CIBER I과 달리 CIBER II는 하나의 주경과 부경으로 구성된 광학계를 4 대의 Imager가 beam splitter를 이용하여 관측하게 구성되어 있다. CIBER II는 NASA에서 공식적으로 승인되었으며, 한국천문연구원과 한국기초과학지원연구원이 미국 NASA/JPL, Caltech 및 일본 ISAS와 국제 공동으로 개발할 계획이다.

• KIISE Transactions on Computing Practices
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• v.23 no.3
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• pp.141-147
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• 2017

Recently there has been an increasing demand for developing a domestic software (S/W) for infrared signature generation to prevent technology leakage and match the domestic operating environment. In this study, we developed a S/W for infrared signature generation and presented its structures and functions for creating and analyzing the IR images of designated spectral bands. The proposed S/W generates IR images of an object through calculations of surface temperatures and IR signals including the self-emitted, surface reflected and path dependent radiances. Moreover, the proposed S/W includes the features of infrared threat analyses from the generated IR images including the infrared contrast radiant intensity (CRI), detection ranges or detection probability analyses, unlike the imported, commercial infrared signature generation S/W.

• Korean Journal of Optics and Photonics
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• v.25 no.5
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• pp.245-253
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• 2014

We report a realistic field-performance simulation for a new MWIR camera. It is designed for early detection of missile plumes over a distance range of a few hundred kilometers. Both imaging and radiometric performance of the camera are studied by using real-scale integrated ray tracing, including targets, atmosphere, and background scene models. The simulation results demonstrate that the camera would satisfy the imaging and radiometric performance requirements for field operation.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.1
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• pp.68.1-68.1
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• 2012

CIBER 2(Cosmic Infrared Background ExpeRiment 2)는 CIBER1의 후속과제로 진행되는 사업으로써 적외선 기기를 NASA Sounding Rocket에 탑재하여 0.5-2.1${\mu}m$ 파장대의 적외선 우주배경복사를 관측하고 실험하는 과제이다. CIBER 2는 NASA에서 공식 승인되어 진행되고 있는 사업이며, 미국의 Caltech, 한국의 KASI, 일본의 ISAS/JAXA가 국제협력으로 진행하는 과제이다. 한국의 KASI는 반사경의 광학계 및 광기계부 개발, 전자부 개발에 참여하고 있다. CIBER 2의 광학계는 카세그레인 방식으로써 주경의 직경은 300mm이다. CIBER 2는 77K로 냉각되어 적외선우주배경복사를 관측하기 때문에 특히, 열수축에 의한 영향을 고려하여 설계, 제작, 조립이 되어야 한다. 또한, 광학계 구조물이 조립되는 로켓의 내경이 400mm이기 때문에 광학계 구조물의 직경에 제한이 따른다. 본 발표에서는 KASI가 주도적으로 개발 중인 반사경 마운트와 광학계 구조물의 초기설계와 광기계 해석결과들에 대해서 논한다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.33 no.6
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• pp.375-382
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• 2020

Owing to the rapid development of infrared guided weapon systems, the threat to aircraft survivability is constantly increasing, and research on infrared stealth technologies are being conducted to ensure aircraft survival. In this study, we analyze the minimum infrared signature of an aircraft according to its flight altitude by considering the characteristics of infrared guided missiles, which detect the contrast signature between the aircraft and background. We conducted computational fluid dynamics simulations for the convective coefficient, and heat transfer simulations were performed considering convection, conduction, and radiation for flight conditions. Thus, we obtained the surface temperature distribution of the aircraft and analyzed the aircraft infrared signature based on the flow characteristics around it. Furthermore, the optimum emissivity for the minimum infrared signature was derived, and the effect of the infrared signature was analyzed when this optimum emissivity was applied to the fuselage surface for each flight condition.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.29.2-29.2
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• 2005

• Bulletin of the Korean Space Science Society
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• 2006.10a
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• pp.100-100
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• 2006