• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.142-147
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• 2009

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be tested under vacuum condition and very low temperature in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels such as north and south panels. They will be controlled from 90K to 273K by circulating GN2 and LN2 alternatively according to the test phases, while the shroud of the vacuum chamber will be under constant temperature, 90K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test.

• 설비공학논문집
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• 제29권9호
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• pp.482-495
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• 2017

Degree-days are practically used as a tool to estimate energy consumption for heating and cooling. Degree-days are calculated by summing differences of balance point temperature and outside temperature for the analyzed period. Determining balance point temperature is a key point in calculating accurate degree-days. However, ASHRAE standards are used for balance point temperature in Korea because balance point temperature considering climate conditions and building thermal performance is not proposed in Korea. This study proposes the process to generate balance point temperature for heating degree-days considering Korean climate and building conditions. Also, a new balance point temperature for three regions in Korea will be suggested in this study. Balance point temperature of Seoul is approximately $15.0^{\circ}C$, lower than the current standard of $18.3^{\circ}C$. Balance point temperature of Seoul considering climate conditions and building performance can be different from the ASHRAE suggested value ($18.3^{\circ}C$). Results revealed the current standard for balance point temperature should be changed considering climate and building conditions in Korea.

• Journal of Astronomy and Space Sciences
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• 제26권3호
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• pp.403-416
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• 2009

한국항공우주연구원에서는 기상탑재체, 해양탑재체 및 통신탑재체를 탑재한 정지궤도 위성인 통신해양기상위성을 개발하고 있다. 한국항공우주연구원에서 자체 개발한 대형 열진공 챔버를 이용하여 통신해양기상위성의 열평형 시험을 수행 할 예정이다. 열평형 시험의 주목적은 열해석 모델을 보정하고 열제어 설계를 검증하는데 있다. 통신해양기상위성의 고온 열평형 시험을 위해 남쪽과 북쪽 방열판 위에 외부 열유입량을 모사하기 위한 히팅플레이트를 장착하고, 액화질소 및 질소가스를 이용하여 히팅플레이트의 온도를 90K에서 260K 사이로 조절할 예정이다. 또한 열진공 챔버의 벽면은 심우주의 낮은 온도를 모사하기 위해 열평형 시험동안 액화질소를 이용하여 90K로 유지할 예정이다. 이 논문에서는 통신해양기상위성의 열평형 시험을 위한 열진공 챔버, 탑재체를 위한 타깃, 히팅플레이트 등 위성 모델링에 관한 내용과 열평형 시험 예측을 위한 경계조건, 부품의 작동 상태 및 온도 예측에 관해 다루고자 한다. 또한 새로이 개발한 히팅플레이트를 이용하여 열평형 시험을 수행하는 방법에 대한 타당성을 검토하고자 한다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2006년도 추계학술대회
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• pp.113-117
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• 2006

This paper Is for development of cooling module in order to maintain heat and water balance in fuel cell vehicle. Thermal management system for fuel cell is disadvantage because the temperature of coolant is lower than that of ICE and heat duty of radiator is higher. By CFD simulation, cool ing module was developed for water balance of system. Hot chamber test and hot area/high altitude test on cool ing module was completed.

• 한국항공우주학회지
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• 제34권12호
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• pp.90-95
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• 2006

위성 열평형 시험에 사용하는 열진공 챔버의 벽은 흑체 거동을 하는 우주공간과는 달리 위성의 복사 에너지를 완벽하게 흡수하지 못하고 일부를 반사한다. 챔버의 크기가 작을수록 이러한 챔버 벽 효과는 커지는 것으로 알려져 있다. 이것은 시험비용을 줄이기 위해 대형 챔버를 사용하기 힘든 소형위성의 개발에 걸림돌이 된다. 본 연구에서는 챔버 벽 효과를 예측하고 이를 보정하기 위한 정량적인 분석을 진행하였다. 그 결과로 챔버 벽 효과에 의한 온도 오차를 계산하여 시험 데이터를 보정할 수 있게 하였다. 또, 최적 면적비를 정의하여 소형위성의 열평형 시험용 열진공 챔버의 크기를 정하는데 기준을 마련하였다. 덧붙여 챔버 벽을 투명한 재질로 코팅하여 챔버 벽 효과를 줄일 수 있는 방안에 대해 이론적인 분석을 수행하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.230-235
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• 2011

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and was developed by KARI for communication, ocean and meteorological observations. COMS was tested under vacuum and very law temperature conditions in order to correlate thermal model and to verify thermal design. The test was performed by using KARI large thermal vacuum chamber. The COMS S/C thermal model was successfully correlated versus the 2 thermal balance test phases. After model correlation, temperatures deviation of all individual unit were less than $5^{\circ}C$ and global deviation and standard deviation also satisfied the requirements, less than $2^{\circ}C$ and $3^{\circ}C$. The final flight prediction was performed by using the correlated thermal model.

• 한국전산유체공학회지
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• 제16권3호
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• pp.59-65
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• 2011

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and was developed by KARI for communication, ocean and meteorological observations. COMS was tested under vacuum and very low temperature conditions in order to correlate thermal model and to verify thermal design. The test was performed by using KARI large thermal vacuum chamber. The COMS S/C thermal model was successfully correlated versus the 2 thermal balance test phases. After model correlation, temperatures deviation of all individual units were less than $5^{\circ}C$ and global deviation and standard deviation also satisfied the requirements, less than $2^{\circ}C$ and $3^{\circ}C$. The final flight prediction was performed by using the correlated thermal model.

• 조명전기설비학회논문지
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• 제26권5호
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• pp.1-12
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• 2012

In order to reduce energy consumption and greenhouse gas emission in building domain, thermal insulation of building is being enhanced. In a well insulated and tightened environment, internal heat gain caused by solar radiation, luminaires, electronic appliances and metabolism can be more important to thermal condition of building. This paper presents mathematical/physical models of quasi-adiabtic room and lighting fixtures using heat balance equation and thermal-electric analogy to quantify and modelize the heat gain due to luminaires. Experimental results are used to identify thermal parameters of theoretical models. And simulation results of models using Matlab/Simulink are conducted to verify the models and to investigate the thermal effect of lighting fixtures into quasi-adiabatic room.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.343-347
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• 2001

Advanced Pressurized Reactor 1400(APR-1400), which is a standard evolutionary advanced light water reactor(ALWR), has been developed from 1992 as one of long-term Government Project(G-7). The APR-1400 is designed to operate at the rated output of 4000MWt to produce an electric power output of around 1450MWe. The balance of plant (BOP) for the secondary system consists of main steam, feedwater, condensate, turbine generator and auxiliary system. In this paper, we describe the major design features of secondary component, balance of plant configuration, and then the turbine cycle thermal performance evaluation using PEPSE code.

• 대한기계학회논문집B
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• 제25권4호
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• pp.451-460
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• 2001

An analysis program for the thermal performance prediction of steam turbine cogeneration systems with multi-extraction, reheat and regeneration has been developed on the basis of the thermodynamic heat balance method. Heat balance analyses were performed for a commercial cogeneration power plant using the program. Its appropriateness was verified by comparing its heat balance results with those of other commercial programs and those provided by the original system designer. Further parametric analyses were carried out and performance improvement measures in designing the plant were suggested.