• The Bulletin of The Korean Astronomical Society
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• v.44 no.1
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• pp.55.2-55.2
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• 2019

한국형 시험용 달 궤도선(KPLO)에 실릴 과학 탑재체 가운데 하나인 광시야 편광 카메라(PolCam)는 최초로 달 표면전체의 편광 특성을 관측한다. 편광 특성은 태양-달-관측기기 사이의 각도인 위상각에 따라 달라지므로, 다양한 위상각에서의 반복 관측을 통해 달 전 지역에 대한 각각의 편광곡선을 얻을 예정이다. 편광곡선으로부터 달 표면의 입자 크기와 성분 등의 분포를 알 수 있다. 이는 과학적으로도 흥미로울 뿐 아니라, 미래의 달 탐사 임무를 위한 착륙지 선정 시에도 중요한 참고자료가 된다. 여기에서는, PolCam이 1년간의 KPLO 임무 동안 관측할 수 있는 지역 및 위상각의 분포를 소개한다. 또한, 임무 도중 관측이 일시중지되거나 임무 자체가 비정상종료되는 경우 불완전한 관측 자료로부터 편광곡선을 구하는 방법에 대해 알아본다.

• Current Industrial and Technological Trends in Aerospace
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• v.9 no.1
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• pp.119-129
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• 2011

The soft landing of a lunar lander after the entrance of lunar orbit is an essential prerequisite for the accomplishment of the lander's lunar mission. During the landing process of a lunar lander, efficient shock absorption and stability maintenance are indispensible technology to protect payloads. Therefore, the landing gear is a crucial structural component of a lunar lander, it has to absorb the kinetic energy associated with touchdown and support the static load of the landing module in an upright position. In this paper, various landing gears of lunar landers which are being developed as well as which had been successfully landed on the moon surface are investigated. In the end, the Korean lunar lander, which is being designed for preliminary development model, is presented as an example of the lunar lander development.

• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.213-220
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• 2013

Korean Lunar Explorer is planned to be launched in the 2020s according to national space development strategy. The Lunar Explorer will be developed as two unmanned light weight models: a lunar orbiter and a lunar lander. The Lunar Explorer's structure should be designed to have light weight due to constraints from launcher as well as to provide structural safety against launch load, in-orbit condition and landing condition and to serve accommodation space for mission equipment. Core technology related to structural development of lunar explorer should be developed in advance. Especially, for lunar lander, technology for developing landing gear which enables lander to land safely on lunar surface is required essentially. This paper deals with structural development of lunar lander ground test model including design, manufacturing and test.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.39A no.4
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• pp.212-214
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• 2014

In this paper, we present the scenario designs of the possibility of space communications for Korean Lunar Explorer and the analysis of its performance, depending upon the explorer's position within the moon's orbit after being launched from earth. As per each scenario, we would like to propose the analysis of the possible communication times and total transmission throughput data per day in two cases: one for using DSN and another for using only Korean's ground station.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.12
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• pp.1018-1024
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• 2013

On-Board computers (OBC) for LEO & GEO satellites have been developed with their own dedicated architecture so far even though they have many similar functionalities. In this paper, we present a conceptual study results of standard OBC architecture design and propose the domestic development plan for the next generation satellite OBC. Proposed architecture is highly flexible and can be used at LEO/MEO/GEO and Moon Explorer/Deep Space Probe. Also, we introduce current status of standard OBC which is under development.