• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.79-84
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• 2010

The supply system module of the liquid rocket engine has been developed, which consists of the various supply system components such as pipes, orifices, elbows, bellows, valves and flanges. This module can size the components and calculate pressure drops between them. For the assembly of the supply system components, the supply system module can evaluate the number of the components, total pressure drop, outlet pressure and total system weight.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.52-57
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• 2012

A liquid rocket system consists of a combustion chamber, a gas generator, a turbo pump, and a turbine, etc. Each component is connected by supply components such as valves, pipes, and orifices. Since each component has a combined effect on engine performance, preliminary analysis for overall system must be required before the conceptual design stage. Comprehensive analysis program considered the supply system has not been developed yet. In this paper, a supply component model of the liquid rocket engine has been designed after verification of each component. The gas generator cycle with supply components has been composed. The results of the cycle has been compared to those of the F-1 engine with the representative gas generator cycle.

• Aerospace Engineering and Technology
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• v.3 no.2
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• pp.116-123
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• 2004

The SINDA/FLUINT program is used as analysis tool. Thermal model and fluid model are applied for reliable results. By this analysis, the global requirements from System requirement review(SRR) is verified, and the detail requirement of each component is investigated. The results of this analysis is used to set up criterion for selecting proper components.

• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.3
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• pp.22-29
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• 2003

The propulsion feeding system of KSR-III is composed of tubes, valves and PSC, and controls the flow of propellant entering to engine. The test of PTA-I is carried out to verify the characteristic of propulsion feeding system and component. The tests of operation characteristic of component, hydraulic characteristic of tubes, flow control using venturi, oscillation of dynamic pressure, characteristic of regulator are carried out. Troubles of component are found out, and renewed, and the performance of the propulsion feeding system is verified through PTA-I. The results of PTA-I are used to the configuration of propulsion feeding system and test of PTA-II.

• 한국신재생에너지학회:학술대회논문집
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• 2010.11a
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• pp.177.2-177.2
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• 2010

전세계 풍력발전 시장은 2009년말 160GW로 지난 5년간 연평균 36.1%로 성장하였으며, 2012년 310GW, 2020년에는 1,900GW에 이를 전망이다. 특히, 풍력산업은 조선, 중공업 등 우리나라가 강세에 있는 산업과 연관성이 높아 관련분야 대기업을 중심으로 시장진출이 활발히 진행되고 있는 추세이다. 본 연구는 지식경제부에서 지원하고 있는 신재생에너지기술개발사업 R&D지원실적을 토대로 풍력산업 및 기술혁신패턴을 분석하고, 이를 토대로 풍력산업 발전을 위한 기술혁신 지원전략을 연구하였다. 분석결과, 풍력시장이 급성장함에 따라 대기업을 중심으로 급진적 혁신 행태을 보였으며, 기술도입 및 선진기술의 모방이라는 전형적인 초기산업화 패턴을 보이고 있다. 이러한 기업전략은 기술혁신체제 관점에서 기술학습을 통한 기술축적이 부족하고, 부품소재 중심으로 공급사슬을 구성하는 중소 중견기업군이 취약하여 원가절감 등 시장 경쟁력에 장애요인으로 나타났다. 이를 개선하기 위해서는 첫째, 시스템 기업은 중소 중견기업을 중심으로 부품국산화 노력을 통한 경쟁력 있는 공급사슬 구현이 시급하다. 둘째, 정부는 부품소재 중심의 원천연구에 대한 지원을 확대하여야 하며 셋째, 경쟁력 있는 국가의 기술혁신체계 구현을 위해 정부 출연연구소 및 대학을 중심으로 기술축적을 위한 방안이 시급하다. 마지막으로 초기 풍력산업의 주요 수요자가 정부 및 공공기관인점을 감안할 때, 풍력시스템의 국산화 비율을 구매 조건의 핵심 평가요인으로 채택해야 할 것이다.

• Proceedings of the Korean DIstribution Association Conference
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• 2006.08a
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• pp.47-68
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• 2006

This study aims to determine the association structure of the behavioral relationship variables, such as trust, commitment, cooperation, communication and coercive power, in the relationship between the buyers and suppliers of industrial parts. It also investigates the impact of the use of IT technologies on the relationships quality. Data was collected from 216 part suppliers of machinery, electronics and automobiles located in Incheon. Data supported all of the proposed hypotheses. First, it was confirmed that parts suppliers' trust in buyers leads to the commitment into relationships with buyers. Second, cooperation and communication showed a positive influence on parts suppliers' trust in buyers, and coercive power gave a negative influence on trust. Third, the use of IT technologies like Internet and E-Mail between parts suppliers and buyers was verified to have generally a positive influence on the quality of relationships. At the same time, cooperation and communication were confirmed to have a positive influence on each other, and cooperation and coercive power as well as communication and coercive power were confirmed to have negative influence on each other. This study is a pioneering attempt to examine the relationships between suppliers and buyers of industrial parts, and the influence IT technologies on the relationship quality. Also, the findings will be practically much helpful to find how to reinforce the relationships between parts suppliers and buyers.

• 유체기계공업학회:학술대회논문집
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• 2006.08a
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• pp.241-244
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• 2006

The analysis of propellant feeding sub-system is performed using a commercial code SINDA/FLUINT, the comprehensive finite-difference, one-dimensional, lumped parameter tool. With the code, cryogenic helium supply system, liquid oxygen supply system, helium injection cooling system are evaluated. The code gave satisfactory estimation scheme for propulsion system characterized by cryogenic temperature and high pressure, two phase flow. This paper focuses on presenting calculation scheme of propulsion sub-system using one-dimensional code like SINDA/FLUINT.

• LP가스
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• v.20 no.2
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• pp.59-67
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• 2008

지난 4월 2일 GAS KOREA 2008 전시회가 개최된 서울무역전시장에서 '한국DME협회 분과발표회'가 열렸다. 이날 분과발표회에서는 'DME Demo 플랜트 현황소개(한국가스공사 연구 개발원 조원준 박사 "DME 연료실증, 시험연구 사업현황(한국가스공사 연구개발원 백영순 박사)" 커먼레일형 연료공급계를 탑재한 2리터급 DME 차량개발(자동차 부품연구원 정재우 박사) "급속압축장치를 이용한 불균일 예혼합기의 DME HCCI연소 과정에 관한 연구(울산대학교 임옥택 교수) DME의 자착화 측정 및 세탄가의 추정(인하대학교 이대엽교수)" 직접분사식 압축착화기관에서 DME연료의 분무미립화 및 배출물 특성(한양대학교 이창식 교수)' 에 대한 발표도 이뤄졌다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.93-97
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• 2010

The energy balance program which can balance the relations among energy, mass flow, pressure in the staged-combustion cycle of the liquid rocket engine has been developed. The modular approach has been chosen for the analysis; the engine cycle consists of the elements from the predefined component analysis program. The engine with the staged-combustion cycle has been decomposed into several principal component modules, such as a thruster chamber, turbopumps, turbines, supply system components and a pre-burner. The program has been verified with comparison of the results to the selected data of the space shuttle main engine.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.15 no.9
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• pp.5480-5486
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• 2014

Complete novel software for MDPS for the simulation and analysis is proposed for steering engineers. The software, MSAS, which can provide the functionality for MDPS Simulation, Analysis & Synthesis, is based on the steering system model, vehicle model and control logic. As the suppliers provide the control logic as a black box, this software is capable of using any type of black box logic or white box control logic that can be developed by logic designers. In addition, this software will be synthesized with the suppliers' s-function control logic and RMDPS together.