• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.1
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• pp.26-34
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• 2019

In this paper, a coarse lunar soil model is developed using discrete element method and its computed physical properties are compared with those of the actual lunar soil for its validation. The surface of the actual moon consists of numerous craters and rocks of various sizes, and it is covered with fine dry soil which seriously affects the landing stability of the lunar lander. Therefore, in consideration of the environment of the lunar regolith, the lunar soil is realized using discrete element method. To validate the coarse model of lunar soil, the simulations of the indentation test and the direct shear test are performed to check the physical properties(indentation depth, cohesion stress, internal friction angle). To examine the performance of the proposed model, the drop simulation of finite element model of single-leg landing gear is performed on proposed soil models with different particle diameters. The impact load delivered to the strut of the lander is compared to test results.

• Journal of Space Technology and Applications
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• v.4 no.2
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• pp.121-136
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• 2024

Korea Pathfinder Lunar Orbiter (KPLO), launched in August 2022, is successfully carrying out its mission. Korea's lunar lander and rover programs are expected to proceed in the future. To successfully carry out the mission after the lunar lander has landed on the surface, the performance of the equipment to be mounted should be checked in a laboratory environment similar to the Moon. Scientists and engineers of several countries, including the United States and China, use lunar soil simulant which is developed to resemble lunar soil for simulating the surface of the lunar landing site. Several lunar probe landing sites are being discussed in Korea, and lunar soil simulants such as Korea Hanyang Lunar Simulant-1 (KOHLS-1), Korea Aerospace University Mechanical Lunar Simulants (KAUMLS), and Korea Lunar Simulant-1 (KLS-1), which are similar to the characteristics of lunar mare soil, have been developed. However, those simulants are not useful if the landing site is chosen as a highland area. In this study, we introduce the process of developing KIGAM-L1, a lunar highland soil simulant similar to the chemical composition of the Apollo 16 lunar soil sample and the particle size distribution of lunar soil sample 60500-1, in case the lunar lander lands at highland area.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.104.2-104.2
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• 2012

미국, 중국, 일본, 인도 등과 같은 세계 여러 국가들이 달 및 화성 탐사를 수행하고 있는 현시점에서 우리나라도 2025년에 달 탐사를 계획하고 있다. 인간에게 있어서 우주공간은 고에너지 환경의 영향을 많이 받는 곳이다. 향후 달, 화성과 같은 다른 행성으로의 이주를 생각하고 있는 현 시점에서 우리는 고에너지우주방사선 환경의 영향을 고려해야 한다. 지구에서의 인간은 지구 자기장과 대기에 의해 고에너지 우주선 환경으로부터의 영향을 덜 받는다. 그러나 달과 화성의 경우는 다르다. 달의 대기는 거의 없고 자기장도 무시할 정도로 매우 작으며, 화성 또한 자기장이 거의 없으며 대기 또한 얇아서 Galactic Cosmic Ray (GCR)나 Solar Energetic Proton (SEP) 등으로부터 인간은 많은 영향을 받을 수 있다. 이러한 위험으로부터 인간이 보호받을 수 있는 곳은 달과 화성의 지표 아래나 동굴이라고 볼 수 있다. 그래서 달 및 화성의 표면과 지하 영역에 대한 고에너지 우주선 환경의 깊이에 따른 영향을 분석하여 어느 정도로 두터운 천장을 가진 동굴이어야 우주인들이 상주하는 지하공간을 지구표면에서의 방사선 환경과 같은 수준으로 유지할 수 있는지를 추정해 보려고 한다. 달 표면 토양의 화학적 구성성분은 Maria와 Highlands로 구분되어 약간의 차이가 있다. 달의 Maria 토양은 $SiO_2$ - 45.4%, $Al_2O_3$ - 14.9%, CaO - 11.8%, FeO - 14.1%, MgO - 9.2%, $TiO_2$ - 3.9%, $Na_2O$ - 0.6%이고 Highlands의 토양은 $SiO_2$ - 45.5%, $Al_2O_3$ - 24.0%, CaO - 15.9%, FeO - 5.9%, MgO - 7.5%, $TiO_2$ - 0.6%, $Na_2O$ - 0.6%의 화학적인 구성비를 가진다. 또한 화성표면은 $SiO_2$ - 43.9%, $Al_2O_3$ - 8.1%, CaO - 6.0%, FeO - 18.1%, MgO - 7.1%, $Na_2O$ - 1.4%의 토양의 화학적인 구성비를 가지고 있다. 본 연구에서는 이러한 구성비를 가지고 있는 달과 화성 표면에 대한 우주방사선의 영향을 분석하기 위해서 GEANT4를 사용하여 수행한 전산 모사의 결과를 발표할 것이다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.12
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• pp.1037-1044
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• 2014

In this study, we designed a drop test system considering lunar surface environment and tested landing gear of experimental lunar lander. The lunar lander would be landed at soil place for soft landing. When the lunar lander touches down, the acceleration of the lander is largely affected by mechanical characteristics of the lunar soil. Accordingly, a drop test using lunar soil is needed to verify the performance of the lunar landing gear. Because the lunar soil is not available generally, we developed a lunar simulant KAUMLS(Korea Aerospace University Mechanical Luna Simulant) based on mechanical properties of the lunar soil of NASA's LUNA PROJECT. In addition, drop tests on steel plate and dry sand are performed to evaluate impact characteristics by the surface environment.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.4
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• pp.284-290
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• 2014

To successfully explore the moon by lunar lander, it is essential to guarantee the safe landing of lunar lander. Therefore, efficient shock absorption system of lunar lander should be designed in order to reduce landing impact force. Also, for more practical design of lunar lander, it is important to consider the effect of lunar regolith. In the line of thought, finite element model of lunar lander considering the effect of lunar regolith is developed. To reduce landing impact force, optimization of shock absorption system for lunar lander has been carried out. In optimization, sequential approximate optimization method based on meta-model is used. Through the result of optimization, it is verified that landing impact force on lunar lander can be efficiently reduced by the present optimization procedure.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.39 no.2
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• pp.327-333
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• 2019

For sustainable lunar exploration, the most required resources should be procured on site because it takes tremendous cost to transfer the resources from the Earth to the Moon. The technologies required for use of lunar resources refers to In-Situ Resource Utilization (ISRU). As the ISRU technology cannot be verified in the Earth, a lunar surface environment simulator is necessary to be prepared in advance. The Moon has no atmosphere, and the average temperature of the lunar surface reaches to $107^{\circ}C$ during the daytime and $-153^{\circ}C$ at night. The lunar surface is also covered with very fine soils with sharp particles that are electrostatically charged by solar radiation and solar wind. In this research, generation of vacuum environment with lunar soil mass in a chamber and simulation of electrostatically charged soils are taken into consideration. It was successful to make a vacuum environment of a chamber including lunar soils without soil disturbance by controlling evacuation rate of a vacuum chamber. And an experiment procedure for simulating the charged lunar soil was suggested by theoretical consideration in charging phenomena on lunar dust.

• Korean Journal of Environmental Biology
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• v.32 no.4
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• pp.363-370
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• 2014

Various ecosystem carry out fundamental function of material circulation and energy flow through interrelationship with many environmental factors. Therefore, it is crucial to scientifically understand the value of nature to deduce correlation between environmental factor and change of ecosystem function. In this study, we determined the accumulated ecosystem carbon and characteristics of soil respiration on grassland vegetation in Namahangang basin in Namhangang Basin. It was found that the rate of soil respiration was highly correlated with the soil temperature in all communities. The measured soil respiration rates were $1,539mgCO_2\;m^{-2}h^{-1}$, $1,200mgCO_2\;m^{-2}h^{-1}$, $1,215mgCO_2\;m^{-2}h^{-1}$ in Miscanthus sacchariflorus, Phragmites japonica, Salix koreensis communities, respectively. Also, carbon quantities accumulated in litter and soil layers were $40.6tCha^{-1}$ (1.9+38.7), $46.9tCha^{-1}$ (43.0+3.9), $31.2tCha^{-1}$ (28.9+2.3) in M. sacchariflorus, P. japonica, S. koreensis communities, respectively.

• Journal of the Korean Institute of Gas
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• v.21 no.1
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• pp.72-79
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• 2017

The operating temperature range of the natural gas pipeline in Arctic environment would be controlled primarily to optimize gas throughput and to minimize the environmental impact resulting from operation of such pipelines. The temperature of the gas as it flows through the pipeline is a function of both the Joule-Thomson effect and the pipe to soil heat transfer. Therefore, the heat transfer and Joule-Thomson effect of the buried natural gas pipeline in this study were carefully considered. Soil temperatures and overall heat transfer coefficients were assumed to be $0{\sim}-20^{\circ}C$ and $0{\sim}5.5W/m^2K$, respectively. The gas temperature and pressure calculations along a pipeline were performed simultaneously at different soil temperatures and overall heat transfer coefficients. Also, this study predicted the phase change and hydrate formation for different soil temperatures and overall heat transfer coefficients using HYSYS simulation package.

• Bulletin of the Korean Space Science Society
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• 2011.04a
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• pp.31.3-31.3
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• 2011

달의 양방향 분포 함수는 Hapke에 의하여 처음 이론적 모델이 만들어졌고, 이후 Foote에 의해 아폴로 11호의 달 토양 샘플 10084의 양방향 분포 함수가 측정된 바 있다. 이 연구에서는 실제 크기의 달의 표면에 Hapke의 양방향 분포 함수를 적용하여 광학 모델은 개발하였다. 달 표면의 산란특성 중 반 무한하고 매끄러운 지면에 적용되는 후방산란 효과와 산란각에 따른 위상 함수가 적용된 모델이 사용되었으며, 위상함수로는 Henyey-Greenstein 함수가 사용되었다. 달의 3D 모델에 사용된 매개 변수는 Foote가 측정한 Hapke의 변수를 따랐으며 달의 단일 산란 알베도는 w=0.33, 핫스팟의 넓이는 h=0.017, Legendre 다항 계수인 b와 c에는 각각 b=0.308, c=0.425의 값이 사용되었다. 구성된 달의 양방향 분포 함수를 이용한 통합적 광선 추적 수치 모사 결과, 달 반사광의 복사 휘도율은 1차 근사 해석적 방법을 이용한 계산 결과의 복사 휘도율과 측정 오차 범위 이내의 오차를 보였다.

• Journal of Animal Environmental Science
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• v.5 no.2
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• pp.113-122
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• 1999

온실에서 퇴비화 발효율을 이용하기 위하여 발효율이 토양을 직접 가온하면서 퇴비화하는 퇴비화 하우스를 제작하였다. 퇴비화가 진행되는 동안 각 단계별 열의 발생량과 발생열량이 토양에 전달되는 특성을 분석하였다. 우분과 왕겨를 혼합하여 퇴비화 처리하였다. 퇴비화 과정의 총 70일 동안 391MJ/㎥의 열량이 발생하였으며, 이중 22일의 주발효기간 동안에 약 82%의 열량이 발생하였다. 또한 총 열량중 토양의 지표면의 지표면을 통하여 방출되는 열량을 제외한 260M/㎥의 열량이 지중가온에 이용된 것으로 나타났다. 콤포스트의 열 전도계수는 1.7~0.3W/m$^{\circ}$K이었다. 퇴비화 시스템을 구비한 온실의 주 발효기간의 지중 평균온도는 27.9$^{\circ}C$인 반면, 퇴비화 시스템이 없는 온실의 경우 13.9$^{\circ}C$로 나타나 퇴비화 시스템이 지중 온도증가에 큰 효과를 나타내고 있었다.