• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.290-295
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• 2003

Among the thermal analysis methods for Multi-Layer Insulation(MLI), effective emittance, diffusion MLI node and arithmetic MLI node methods are compared. The methods have been applied to the aluminum panel under the low earth orbit environment. TRASYS program is used for geometrical math modeling and SINDA program for thermal math modeling and temperature calculation. Test cases are selected according to MLI area on the panel. Temperature results are calculated and compared under the ratio of absorptivity and emissivity.

• 한국수소및신에너지학회논문집
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• 제31권6호
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• pp.571-577
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• 2020

Thermal analysis was performed for a cold box of a hydrogen liquefaction pilot plant with 0.5 ton/day capacity. The pilot plant has adopted a hydrogen liquefaction process using two-stage helium Brayton cycle with precooling of liquid nitrogen. The cold box for hydrogen liquefaction has generally vacuum insulation but inevitable heat invasion by conduction and radiation exists. The heat loads were calculated for cold box internals according to multilayer insulation emissivity. Total heat load of 181.7 W is estimated for emissivity of 0.03 considered in field condition.

• 한국수소및신에너지학회논문집
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• 제29권4호
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• pp.386-392
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• 2018

Fuel cells are known as eco - friendly energy facilities that can use heat energy and electric energy at the same time. Fuel cells are classified according to the temperature and material used, and solid oxide fuel cell (SOFC) is relatively high temperature ($700-800^{\circ}C$). SOFC requires a hot box consisting of a high temperature stack, a reformer, a burner, and the heat exchangers in order to use energy efficiently. The hot box needs to maintain heat insulation performance at high temperature to reduce heat loss. However, Fibrous insulation, which is widely used, needs to be improved because it has a disadvantage that the thermal conductivity is rapidly increased due to the increase of temperature. Therefore, this study was carried out to develop a thermal insulation, which is applied to multiple layers insulation (MLI) technic, that can be used under SOFC operating conditions and prevent a drastic drop in thermal conductivity at high temperature. The developed insulation is consist of a thermally conductive material, a spacer, and a reflective plate. The thermal conductivity of the insulation was measured by in the thermal conductivity measuring device at high temperature range. As a result, it was confirmed that the developed layers insulation have an good thermal conductivity (0.116 W/mK) than fibrous insulation (0.24 W/mK) as a radiation shielding effect at a high temperature of 1,173 K.

• 한국항공우주학회지
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• 제37권8호
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• pp.798-804
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• 2009

(주)쎄트렉아이는 400kg 급 지구관측 위성의 주 탑재체로 사용될 고해상도 전자광학카메라, EOS-C 시스템을 개발 중이다. 이 시스템은 DubaiSat-1 위성의 주 탑재체 개발을 통해 획득한 경험을 토대로 보다 향상된 광기계 및 열적 성능을 갖도록 설계되었다. 민감한 광학부품의 운용상 성능을 유지하기 위해 히터를 이용한 능동 열제어 방식이 적용되었고, 이와 더불어 히터 소모 전력을 최소화하기 위해 열 코팅 및 다층박막단열재(MLI)를 사용한 수동 열제어 방식이 적용되었다. 열해석 모델을 이용해 임무궤도에 대한 열해석을 수행하였으며, 해석 결과를 바탕으로 이 시스템의 열제어계가 설계 요구조건을 만족하는 것을 확인하였다.