• 한국신재생에너지학회:학술대회논문집
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• 2006.06a
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• pp.233-236
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• 2006

In this paper, I try to measure characteristic transmission-reflection by environmental change or solar cell. I keep my eye on the characteristics variation of solar cell as environmental change. As a result, A variation caused by voltage by an effect on the efficiency of solar PV cell. Hence, it is an important variable when a designer plan to make a solar cell.

• Journal of Aerospace System Engineering
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• v.14 no.3
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• pp.51-59
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• 2020

In the case of cubesat, a PCB-based deployable solar panel advantageous in terms of weight reduction and electrical circuit design is widely used considering the limited weight and volume of satellites. However, because of the low thermal conductivity of PCB, there is a limit relative to heat dissipation. In this paper, the thermal gap pad is applied to the contact between the PCB-based solar panel and the aluminum stiffener mounted on the outside of the panel. Thus, the heat transfer from the solar cell to the rear side of the panel is facilitated. It maximizes the heat dissipation performance while maintaining the merits of PCB panel, and thus, it is possible to improve the power generation efficiency from reducing the temperature of the solar cell. The effectiveness of the thermal design of the 6U cubesat's deployable solar panel using the thermal gap pad has been verified through on-orbit thermal analysis based on the results, compared with the conventional PCB-based solar panel.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.1
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• pp.45-50
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• 2013

The reflector of infrared lamp is designed to the optimal circular shape through the analyses of lumination distributions with a triangular, rectangular and circular configurations of infrared lamps respectively by using Photopia. PLC is used to compare and amplify the difference between soldering temperature profile and feedback value. It is fed to IR lamp controller which adjusts the soldering temperature of PV cell. The soldering temperature measured using an infrared temperature sensor is then fed back to the PLC. The closed control loop of soldering temperature on a PV cell is implemented. The noncontact soldering device of PV cells using infrared lamp which is easily operated by HMI operation panel and controlled robustly by PLC and IR lamp controller is developed.

• 한국신재생에너지학회:학술대회논문집
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• 2006.06a
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• pp.206-209
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• 2006

In this paper, I try to measure the electrical characteristics of PV cell for lanterns with solar simulator and simulated with PC1D software. I keep my eye on the characteristics variation of PV cell as a temperature change. Therefore, I try to increase a temperature of controlled block from $10^{\circ}C$ to $50^[\circ}C$ while measuring the FV cell. As a result, A variation caused by voltage have an effect on the efficacy of PV cell. Hence it is an important variable when a designer plan to make a solar cell for lanterns.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.319-319
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• 2010

칼코젠계 태양전지의 광흡수층으로 사용되는 CuInSe2은 직접천이형 반도체로 광흡수계수가 $1{\times}105cm-1$로 매우 높고, 전기광학적 안정성이 우수하여 실리콘 결정질 태양전지를 대체할 고효율 태양전지로 각광받고 있다. 광흡수층의 밴드갭 에너지가 증가하면 태양전지의 개방전압(Voc)이 증가하여 광변환 효율을 향상시킬 수 있으므로, CuInSe2에서 In의 일부를 Ga으로 치환하여 에너지 밴드갭의 변화를 주는 연구가 많이 진행되고 있다. 그러나 화합물내의 Ga 조성비가 증가하면 단락전류(Jsc), 충진률(fill factor)이 낮아져 태양전지 효율을 저하시키게 되므로 CIGS 박막의 적절한 화합물 조성비를 갖도록 최적조건을 확립하는 것이 매우 중요하다. 본 실험에서는 광흡수층 형성을 위해 Sputtering법으로 금속 전구체를 증착하고, 고온에서 셀렌화 열처리를 수행하는 Sequential process(2단계 증착법)를 이용하였다. soda-lime glass 기판에 Back contact으로 Mo를 증착하고, 1단계로 CuIn0.7Ga0.3 조성비의 타겟을 이용하여 Sputtering법으로 $0.5{\sim}2{\mu}m$ 두께의 CIG 전구체를 증착하였다. 2단계로 CIG 전구체의 셀렌화열처리를 통하여 CIGS 화합물 구조의 박막을 형성시켰다. 이때 형성된 CIGS 화합물 박막의 두께는 동일하게 함으로써, 열처리온도에 의한 박막의 구조변화를 비교하였다. 증착된 CIGS 박막은 고온 엑스선회절분석을 통해 증착 두께와 온도 변화에 따른 CIGS 층의 구조 변화를 확인하고, 동일한 증착조건으로 Buffer layer, Window layer, Grid 전극을 형성하여 태양전지셀 특성을 평가함으로써 CIGS 태양전지 광흡수층의 결정구조에 따른 광변환 효율을 비교하였다.

• Proceedings of the KIEE Conference
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• 2006.07b
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• pp.1199-1200
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• 2006

In this paper, I try to measure the electrical characteristics of PV cell for lanterns with solar simulator and simulated with PC1D software. I keep my eye on the characteristics variation of PV cell as a temperature change. Therefore, I try to increase a temperature of controlled block from $10^{\circ}C$ to $50^{\circ}C$ while measuring the PV cell. As a result, A variation caused by voltage have an effect on the efficacy of PV cell. Hence, it is an important variable when a designer plan to make a solar cell for lanterns.

• Proceedings of the KIEE Conference
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• 2006.07b
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• pp.1201-1202
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• 2006

In this paper, I try to measure characteristic transmission-reflection by environmental change or solar cell. I keep my eye on the characteristics variation of solar cell as environmental change. As a result, A variation caused by voltage by an effect on the efficiency of solar PV cell. Hence, it is an important variable when a designer plan to make a solar cell.

• Proceedings of the Korean Institute of IIIuminating and Electrical Installation Engineers Conference
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• 2006.05a
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• pp.233-236
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• 2006

In this paper, I try to measure the electrical characteristics of PV cell for lanterns with solar simulator and simulated with PC1D software. 1 keep my eye on the characteristics variation of PV cell as a temperature change. Therefore, I try to increase a temperature of controlled block from $10^{\circ}C\;to\;50^{\circ}C$ while measuring the PV cell. As a result A variation caused by voltage have an effect on the efficacy of PV cell. Hence, it is an important variable when a designer plan to make a solar cell for lanterns.

• Journal of Aerospace System Engineering
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• v.16 no.5
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• pp.86-93
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• 2022

Generally, a deployable solar panel is used primarily to achieve sufficient power output to perform the mission. However, temperature distribution on the antenna reflector may increase due to the shading effect induced by the presence of the deployable solar panels. Appropriate thermal design is critical to minimize the thermal deformation of the mesh antenna reflector in harsh on-orbit thermal environments to ensure remote frequency (RF) performance. In this paper, we proposed a dual-surface primary reflector consisting of a mesh antenna and a flexible fabric membrane sheet. This design strategy can contribute to thermal stabilization by using a flexible solar panel on the rear side of membrane sheet to reduce the temperature distribution caused by the deployable solar panel. The effectiveness of the mesh antenna design strategy investigates through on-orbit thermal analysis.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.5
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• pp.423-429
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• 2014

Passive attitude stabilization methods using the permanent magnet combined with hysteresis damper and the gravity gradient boom have been widely used for the attitude determination and control of cube satellite, due to its advantage of system simplicity. In this paper, on-orbit thermal characteristics of the cube satellite considering the attitude profiles obtained from the above passive attitude stabilization methods have been investigated through on-orbit thermal analysis. In addition, the effectiveness of the various thermal coatings on the panel for the communication antenna installation has been verified.