• Journal of Space Technology and Applications
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• v.1 no.2
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• pp.149-159
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• 2021

This paper represents a reentry time prediction analysis of CZ-5B rocket-body in China, subject to analysis of the Inter-Agency Space Debris Coordination Committee Reentry (IADC) reentry test campaign conducted in May 2021. Predicting the reentry of space objects is difficult to accurately predict due to the lack of accurate physical information about target, and uncertainty in atmospheric density. Therefore, IADC conducts annual re-entry campaigns to verify analysis techniques by each agency, and the Korea Aerospace Research Institute has also participated in them since 2015. Ballistic coefficient estimation method proposed to predict target reentry time and the result confirmed the difference of 73 seconds, which confirms the accuracy of the proposed method.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.2
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• pp.156-165
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• 2015

A survivability-analysis program has been developed to analyze the ground collision risk of atmospheric reentry objects, such the upper stages of a launch vehicle or satellites, which move at or near the orbital velocity. The aero-thermodynamic load during the free fall, the temperature variation due to thermal load, and the phase shift after reaching the melting point are integrated into the 3 degree-of-freedom trajectory simulation of the reentry objects to analyze the size and weight of its debris impacting the ground. The analysis results of the present method for simple-shaped objects are compared with the data predicted by similar codes developed by NASA and ESA. Also, the analysis for actual reentry orbital objects has been performed, of which results are compared with the measurement data.

• The Journal of the Korea Contents Association
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• v.18 no.7
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• pp.138-152
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• 2018

The purpose of this study is to investigate that effect of the social support to individual desire of reemployment and satisfaction to reemployed works of career interrupted women. We surveyed about 400 career interrupted women living in Seoul who quit their job within 3 years, analyzed collected data with empirical analysis, and applied structural equation analysis to verify the assumed model for this study. The results of this study showed that social supports influence career interrupted women's individual desire of reemployment, satisfaction to their work, and self-esteem. And the results also showed that the desire of reemployment performs a parametric role between social supports and satisfaction of reemployment. As a consequence, this study showed importance of social supports to reemployment of career interrupted women and satisfaction to their reemployment, therefore, can be helpful to build public policies to promote social manage of women resources.

• Proceeding of EDISON Challenge
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• 2016.11a
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• pp.49-54
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• 2016

본 연구에서는 유/무인 우주발사체의 재진입모듈에 적용되는 Heat-Shield(열차단막)의 형상에 따른 유동특성을 수치해석으로 분석했다. 재진입모듈이 지구의 대기권을 다시 진입하는 환경(고도 70km)을 기준으로 해석을 진행했다. 열차단막의 형상은 평판, 곡률이 다른 타원으로 나누었으며, 각 형상별 유동특성을 확인했다. 결론적으로 재진입 모듈의 형상에 따라 압력과 속도분포를 기준으로 열적인 분포를 예상했으며, 계산된 항력계수를 비교했다. 단순한 유동으로 열적 분포를 예상한 것에 한계가 있지만 대기권 재진입 모듈의 2차원 설계에 도움이 될 형상기준을 제시했다. 수치해석은 모두 Edison_CFD에서 제공하는 툴을 이용해 수행했으며, 전처리에는 e-mega (structured)을 후처리에는 e-dava를 이용했다. 해석 solver는 '정렬격자기반 2차원 압축성 유동 범용해석 소프트웨어'를 이용했다.

• Journal of the Korean Institute of Telematics and Electronics S
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• v.36S no.5
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• pp.21-29
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• 1999

이동횟수 기반 위치갱신 기법에서 고정망과의 접속은 단말 내부의 계수기가 이동횟수 임계치에 이르러 위치갱신이 수행되거나 신규호가 발생할 경우에 행해진다. 그러나 단말의 계수기가 임계치에 이르는 동시에 단말이 이전 위치갱신이 수행된 셀(중앙셀)로 재진입이 발생할 경우 불필요한 위치갱신이 수행된다. [2]에서는 중앙셀로 재진입이 발생하는 경우의 불필요한 위치갱신 수행을 제거하기 위해 중앙셀로 재진입이 발생할 경우 계수기를 영으로 초기화한다. 본 논문에서는 [2]의 기법을 일반화하여 위치갱신 비용을 절약할 수 있는 개선된 기법을 제안한다. 본 기법은 단말이 셀 사이를 이동하는 동안 단말은 자신이 방문한 셀과 이동횟수에 관한 정보를 저장한다. 단말이 이미 방문한 셀로 재진입이 발생할 겨우 이동횟수 계수기를 증가시키는 것이 아니라 이전 방문시 저장하였던 이동횟수로 재조정한다. 이러한 이동회수 계수기의 재조정 방법을 통하여 불필요한 위치갱신과 신호절차를 효과적으로 줄일 수 있다. [2]의 기법은 본 논문에서 제안하는 기법 중에서 중앙셀로 재진입할 때만 계수기를 영으로 재조정하는 특수한 경우에 해당된다. 본 기법이 전체 위치관리 비용을 크게 절약할 수 있음을 증명하기 위해 다양한 환경에서의 성능분석 및 수치적 결과를 통해 알아 본 결과 호 도착 비율당 전체 위치관리 비용이 평균 17-26% 절약됨을 관찰할 수 있었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.4
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• pp.352-362
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• 2016

In this paper, a disposal maneuver which complies the space debris mitigation guideline was analysed for KOMPSAT-2 as an example of LEO satellite. Definition of disposal altitude which comply the '25 year rule', re-entry survivability analysis of KOMPSAT-2 parts inside and casualty area analysis were performed using STK and ESA's DRAMA. Finally, assuming that there were several survival objects during uncontrolled re-entry stage, the re-entry initial orbit elements which show the low casualty probability were found even if there were various uncertainties about the initial orbit. As a result, KOMPSAT-2 should be descended its altitude at least 43km or up to 105km to comply '25 year rule' and there were heavy or heat resistant survival objects which generated $4.3141m^2$ casualty area. And if RAAN of re-entry initial orbit was 129 degree, total casualty probability was lower than standard value of space debris mitigation guideline even if there were uncertainties about the initial orbit.

• Proceedings of the Korean Operations and Management Science Society Conference
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• 2000.04a
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• pp.265-267
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• 2000

가공물을 한 개씩 작업하는 단일작업기계와 여러 개의 가공물을 한꺼번에 작업하는 배치 기계를 포함한 재진입 라인 시스템에서 각 기계가 고장이 일어날 수 있고, 불량품이 발생할 때, 이 시스템에서의 가공물의 생산주기를 구하는 방법을 Mean Value Analysis(MVA)를 이용하여 제시하고자 한다. 배치 기계와 고장 발생, 불량품 발생 등의 이유의 이런 시스템은 승법형 대기행렬 모형으로 모형화 할 수 없다. 본 논문에서는 각 기계에서의 체류 시간을 구하여 전 시스템의 생산 주기를 구하는 방법을 MVA 를 이용하여 제시한다.

• Aerospace Engineering and Technology
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• v.13 no.1
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• pp.184-192
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• 2014

In this paper, the lifetime of the artificial space objects in the LEO is analysed by using TLE data, which is provided by JSpOC. We observed the change of the number of space objects from 1957 and determined the reason of space debris generation. And then, we performed the analysis about present condition of space debris environment. The lifetime analysis includes a total of 11,792 artificial space objects and performed until the year 2050 by orbit propagation. We analyze the annual reentry frequency for the high RCS objects such as nonoperational satellites and rocket bodies, which have the possibility of earth ground impact through STK/Lifetime Tool for accurate and effective calculation. The results show that 9 payloads or rocket bodies will be decayed annually and 2 or 3 objects of total value have the possibility of ground impact. In addition, it is also shown that the 40% of a total analysed objects have the lifetime over 200 years.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.2
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• pp.158-164
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• 2014

LEO(Low Earth Orbit) Satellite which is discarded should be reentered to atmosphere in 25 years by '25 years rule' of IADC(Inter-Agency Space Debris Coordination Committee) Guidelines. If the parts of satellite are survived from severe aerothermodynamic condition, it could damage to human and property. South Korea operates KOMPSAT-2 and STSAT series as LEO satellite. It is necessary to dispose of them by reentering atmosphere. Therefore this paper analyze the trajectory, survivability, casualty area and casualty probability of a virtual LEO satellite using ESA(European Space Agency)'s DRAMA(Debris Risk Assesment and Mitigation Analysis) tool. As a result, it is noted that casuality area is $15.2742m^2$ and casualty probability is 5.9614E-03 then will be survived 198.831kg.

• Korean Journal of Social Welfare
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• v.65 no.3
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• pp.183-206
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• 2013

Using Korean Labor and Income Panel Study (wave 1~11) database, this study analyzed the poverty duration of the poor as a whole and by households' characteristics. For this purpose, I first estimated poverty exit rates and reentry rates applying discrete-time hazard model to the sample, and then calculated poverty duration combining these two probability rates. The results show that about a half of poor households are transitory (short-term) poor with 1~2 years of poverty duration. A quarter is chronic (long-term) poor lasting for 5 or more years of poverty duration. The remained quarter can be categorized as the recurrent or mid-term poor. The socioeconomic characteristics of households greatly affect poverty duration. Long-term poverty is prevalent among female-head households, elderly households, single households, or households headed by a person with a lower level of education. If households' heads do not work, or work as temporary or daily-employed workers, the poverty duration tends to be longer. The findings suggest that the poor consist of various social classes with different characteristics. Efficient anti-poverty policy should be based on thoroughly identifying the specific characteristics and needs of each class.