• Land and Housing Review
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• v.12 no.1
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• pp.129-137
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• 2021

External shading devices are well known solar control devices that can help reduce the cooling load of commercial buildings. For this study, experiments were conducted to examine the feasibility of shading devices in reducing both the cooling and heating loads. The influence of sky radiant cooling during winter was verified for the external shading device, internal roller blind, and window. Results can be summarized as follows. The temperature difference between the inner and outer surfaces of the window with the external shading device was 11.8℃ compared to 14.6℃ for one without the external shading device. This 2.8℃ difference was due to heat exchange by sky radiation when the surface temperature of the shading device was lower than the ambient outdoor air temperature. The roller blind resulted in a lower temperature of 0.8℃ compared to the average temperature of the window's air cavity. This was due to heat exchange by sky radiation of the roller blind surfaces. Without shading devices, the outside surface temperature of the window is about 3℃ higher. The study also found that when external shading devices were installed on both the southwest and southeast sides, the outside surface temperature of the windows were lower on the southwest side than the southeast side.

• Fire Science and Engineering
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• v.23 no.2
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• pp.111-116
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• 2009

17 kinds of fire resistant paint which are currently used were painted on the MDF(middle density fiber board), which suitable to the regulation of Fire Service Act. And we investigate a ignition delay effect under a exposure condition of radiative heat of fire. Radiative heat flux was controlled from $10kW/m^2$ to $30kW/m^2$ using the cone heater. Ignition time, ignition type and surface temperature of the sample were measured. Based on the experimental result, critical heat flux of the fire resistant paint treated sample was $10kW/m^2$ and there were no ignition delay effect above the $30kW/m^2$. And it was found that it will be difficult to expect the fire resistant effect above $400^{\circ}C$ of sample surface temperature.

• Fire Science and Engineering
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• v.22 no.2
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• pp.30-37
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• 2008

We have performed the inflammability test for various flooring materials through a radiant heat panel tester by using the specification KSISO 9239-1 (an examination method of flooring materials) that has been set as an international standard for the fire prevention means of interior flooring materials. We have measured the flame spread distance, critical heat flux and smoke density generated by the fire of various flooring materials while using the radiant heat panel tester. The measurement result has shown the burning characteristics different from each other by the respective flooring materials and we could see that the surface materials and construction elements influence greatly on the heat release and smoke generation. We could see that the evaluation method above is an important test method in evaluating the critical heat flux, smoke generation and flame spread distance that are Important factors in studying for fire risks and it is judged that setting and applying a fire evaluation method of flooring materials suitable for the domestic construction use would be relevant.

• The Bulletin of The Korean Astronomical Society
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• v.35 no.2
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• pp.56.1-56.1
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• 2010

MIRIS(Multipurpose InfraRed Imaging System)는 과학기술위성 3호의 주 탑재체로서 2011년 발사예정인 다목적 적외선 카메라 시스템이다. MIRIS는 우주관측 카메라와 지구관측 카메라로 구성되어 있으며, 우주관측 카메라는 $0.9-2.0{\mu}m$ 영역에서 3.67 deg. x 3.67 deg. FOV로 우리 은하평면 survey 관측과 우주배경복사(CIB) 관측을 수행할 것이다. 현재 MIRIS는 비행모델 개발 마무리 단계에 있으며, 검교정 시험, 열-진공 시험, 진동 시험 등을 수행하고 나면 2010년 말 위성 본체와의 조립을 진행할 것이다. 우주관측 카메라는 궤도상에서 태양, 지구의 적외선 복사와 망원경과 검출기 주변에서 발생하는 열잡음을 줄이기 위해 냉각이 필요하며, 제한된 위성의 무게와 부피, 전력등의 요구조건들 때문에 망원경 및 구조체의 복사냉각(Passive Cooling) 방법을 선택하였다. Passive cooling으로 우주관측 카메라의 망원경이 200K 이하로 냉각되면, dewar에 설치된 소형 냉각기를 가동하여 적외선 센서를 80K로 냉각한다. 위성체 내벽과 우주관측카메라의 각 구조체들 사이의 복사를 차단하기위해 30층의 MLI를 적용 하였고, 각 구조체들간의 열전도를 최소화하기위해 GFRP supporter를 적용하였다. 이 실험은 천문(연)에서 자체 제작한 열-진공 챔버를 활용하여 진행하였으며, 이미 인증모델에 대한 passive cooling 실험을 두 차례 실시하였고, 그 실험 결과를 반영하여 최종 비행모델에 대한 실험을 수행하였으며, 그 실험 결과에 대해 논의 하고자 한다.

• Fire Science and Engineering
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• v.25 no.6
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• pp.104-111
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• 2011

Aluminum has been widely used as frame materials in the curtain walls. Recently, use of steel as a curtain wall frame is being considered due to its higher strength and thermal resistance than aluminum. In this study, fire tests on the basis of EN 13830 were performed with aluminum and steel-aluminum hybrid curtain walls. From the tests, fire resistance integrity, thermal insulation, and radiation properties were evaluated for both systems and compared. According to the test results, the steel-aluminum hybrid curtain wall showed better fire-performance than the typical aluminum curtain wall for the fire resistance integrity and radiation properties. Although, the fire resistance performance for the insulation property was 6 min for both the two frames, the collapses were occurred at 36 min for the steel-aluminum hybrid curtain wall and at 13 min for the aluminum hybrid curtain wall.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.119-119
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• 2013

5년 동안 진행된 고진공 펌프 개발 사업의 일환으로 맥동관형 냉동기에 활성탄 어레이를 장착한 흡기구 직경 14인치 국산 크라이오펌프 완제품이 만들어졌다. 이미 지난해에 완성한 시제품을 가지고 모든 배기성능시험을 완료하고 목표를 뛰어 넘는 성능을 가지고 있음을 입증하였지만 완제품의 경우는 현장에서 스퍼터링 공정에 대한 신뢰성과 열적 내구성 시험이 중요한 항목으로 대두되었다. 개발된 펌프를 생산 공정에 직접 투입하는 모험을 하지 않으면서도 신뢰성을 확보하는 방편으로 카이스트 나노종합팹 센터에서 가동중인 스퍼터링 장비에 완제품을 달고 기존 공정과 같은 방식으로 장치를 운영하면서 외제 상용품을 사용했을 때와 진공성능 및 공정수율을 비교하는 시험을 수행하였다. 또 내구성 시험 항목으로 열부하 시험과 열 사이클 시험을 수행하였다. 열부하 시험은 300도까지 온도를 올릴 수 있는 열판을 펌프 흡기구 배플 앞에 설치하여, 냉동기 2차 냉각단 온도가 20 K 이하로 유지될 수 있는 최대 허용 복사열을 측정하는 방식으로 진행되었으며 열 사이클 시험은 크라이오 펌프의 활성화 기능을 활용하여 완전 활성화(full regen., 10K-300K-10K) 과정을 10회 연속 시행하여 펌프의 배기성능과 기계적 이상 유무를 관찰하였다.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.12 no.3
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• pp.71-74
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• 2012

We have manufactured a close range Dicke type radiometer which consists of two stage low noise amplifier and diode detector. Frequency range of this system is 35 GHz. And this is used for studying temperature calibration on specific objects. We have present millimeter-wave radiometer's thermal calibration method and its characteristics. From absolute temperature 299K to 309K, in proportion to increase temperature, output voltages are linearly increased. In this case, undefined objects can be measured thermal noise temperature relatively. Overall from absolute temperature 214K to 309K, we have obtained relation of temperature and output voltage;V= 0.03601K - 10.70517.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.23 no.1
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• pp.54-60
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• 2011

Procedures for estimation of insulation thickness for a horizontal pipe for condensation control or personnel protection has been investigated, parallel to the previous work of a vertical wall case. Parameters include pipe diameter, emissivity, thermal conductivity, and operating temperatures. The results indicated that the surface emissivity plays a very important role in the design of insulation, specially for the case of high temperature application with low Bi. The effect of surface radiation in such case could be up to 65% of the total. Required insulation thickness for the surface temperature control increases as pipe diameter increases and as surface emissivity decreases. Adequate revision of specifications or standards to include newly invented insulation materials with high emissivity has been also suggested.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.5-5
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• 1998

수정된 연소 반응 함수를 이용하여 복사 열속 교란에 대한 연소 반응 특성을 살펴보았다. Catalyzed DB N5 추진제의 연소 반응을 살펴보기 위하여 Son 등의 실험 결과와 비교하였다. Son 등의 연소 반응 함수는 물리적으로 타당하지 않은 활성화 에너지에서 실험 결과를 예측하였지만, 수정된 연소 반응 함수는 비슷한 추진제의 실제 활성화 에너지 범위에서 복사 열속에 대한 연소율의 반응을 비교적 잘 예측할 수 있었다. 이것은 Son 등에 의해 과소 평가된 복사 열속(f, J)의 영향이 고려되었기 때문인 것으로 판단된다. 민감 변수(sensitivity parameter)들을 구하기 위하여 Ibiricu 등이 제시한 정상 연소 관계식을 이용하였다. AP계 추진제의 표면 온도에 대한 정상 연소율 변화를 살펴본 결과 Zanotti의 AP2 추진제의 실험 결과와 정성적으로 비슷한 경향을 나타내었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2001.11a
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• pp.68-69
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• 2001