• Proceedings of the KIPE Conference
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• 2007.07a
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• pp.46-48
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• 2007

위성체의 전력계 서브시스템은 임무기간 중 탑재체 및 위성체 버스의 각 서브시스템으로 전력을 제어하고 분배한다. 과학기술위성 2호의 전력계 서브시스템은 태양에너지를 전기에너지로 변환하는 태양전지판, 에너지 저장을 위하여 재충전이 가능한 배터리, 그리고 태양전지판으로부터 배터리를 통해 다른 장치에 전력을 전달하는 전력조절 및 제어시스템으로 구성된다. 본 논문은 과학기술위성 2호의 전력계 서브시스템의 구성과 상세설계사양에 관하여 설명한다.

• Journal of Space Technology and Applications
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• v.1 no.1
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• pp.76-84
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• 2021

Because solar panels of normal satellites are faced to the sun, the power generation by the Earth Albedo is almost neglected in satellite's power analysis. However, many cubesats don't have deployable solar panels and in this case the Earth Albedo is not negligible because solar panels are in six sides facing different directions. In this paper, we calculated satellite's power generation by the Earth Albedo. We divided the Earth's surface into grids based on polar coordinate system. We modeled power generation in each solar cell by reflection on these grids. We simulated 1 U cubesat which flies in sun synchronous orbit and 500 km altitude so that we calculated satellite's power generation by the Earth Albedo.

• Bulletin of the Korean Space Science Society
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• 2005.10a
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• pp.57-57
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• 2005

• Bulletin of the Korean Space Science Society
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• 1995.10a
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• pp.13-13
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• 1995

• The Bulletin of The Korean Astronomical Society
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• v.34 no.1
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• pp.104.2-104.2
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• 2009

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.382-384
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• 2013

해상 해수면에서 운영되는 등부표의 한정된 면적과 공간에서 전력공급을 할 수 있는 한계가 있다. 정보통신기술(ICT) 발달로 e항로표지, 집약관리시스템등 해양교통시설에 최첨단 기술 접목으로 등부표에 소비전력연동시스템 증가로 인해 절대적인 전력량이 부족하다. 이러한 문제를 해결하기 위하여 비바람으로 인한 사방팔방 격동, 격랑, 회전 요동으로 직달 및 산란광을 태양 전지판에 최대로 입사할 수 있도록 태양의 이동궤적에 따라 자동추적되는 신 구조의 다면구체형 태양광 발전시스템을 개발하였다.

• Proceedings of the Korean Environmental Sciences Society Conference
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• 2016.10a
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• pp.273-273
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• 2016

• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.4
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• pp.2966-2970
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• 2015

Recently, solar light power generation is widely extended by support policy to regeneration energy. However generation efficiency is decreased when solar module maintain higher than certain point temperature. Therefore, it is need to maintenance under certain point temperature. An method of solving this problem, this paper is developed geothermal exchanger for efficiency improvement of solar cell module. Geothermal exchanger consisted of heat absorber of solar cell module and heat conductor and radiator. Heat of solar cell module is radiated in the earth by geothermal exchanger. An a result, geothermal exchanger is increased generation amount of solar cell module and experiment result showed costs to about 36% increment of generation power.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2005.05a
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• pp.957-961
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• 2005

A satellite component must withstand vibration caused when launch vehicle acoustics and engine rumble transfer to it through its structural mount. Components shall be subjected to environmental tests after manufacturing process thus the environmental test conditions are needed for component level test including vibration and shock. This paper deals with derivation of component-level environmental test specifications, especially for solar panels of STSAT-2(Science & Technology SATellite-2). Sine sweep random vibration, and shock test conditions were generated for solar panels by assuming the satellite as single-degree-of-freedom system with a base excitation.

• Bulletin of the Korean Space Science Society
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• 2006.10a
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• pp.130-130
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• 2006