• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.82-85
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• 2009

In the development of Liquid Rocket Engine(LRE) systems, it is essential to understand the spray characteristics which influence mainly the performance and the stability of combustion. The injectors for this study have a recessed Liquid-swirl/Gas-centered jet coaxial type. For the similarity with actual conditions, the experimental conditions are calculated by using the momentum ratio as a matching parameter, and the stimulants of fuel and oxidizer are gaseous nitrogen and water respectively. The spray fields were measured by means of a photographic technique. Moreover, an effect of the momentum ratio has been investigated.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.150-155
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• 2010

Liquid rocket injectors play crucial roles on propulsive performance, combustion stability, and heat transfer characteristics. Nevertheless, their developments have mainly relied on empirical methods and expensive hot-firing tests due to lack of fundamental understanding of high pressure combustion phenomena in the near-injector regions. The present study was motivated by recent efforts to develop reliable modeling of liquid rocket combustion. The turbulent combustion model based on the flamelet concept has been extended to take into account real-fluid behaviors occurred at supercritical pressures, and validated against measurements for a cryogenic nitrogen injection, a non-premixed turbulent jet flame at atmospheric pressure, and a LOx/$GH_2$ coaxial shear injector at a supercritical pressure.

• The Transactions of the Korean Institute of Electrical Engineers
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• v.38 no.7
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• pp.511-523
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• 1989

This paper investigates physical properties, the electrical and mechanical characteristics of the epoxy resin with different curing methods and postcuring conditions at room temperature or cryogenic temperature (LN2). According to the results in this paper, first, it is found that the physical properties, electrical and mechanical characteristics of the epoxy resin are largely affected by the interior reaction temperature on the curing. Thus, in the fabrication of the sample, several excellent characteristics of the sample are obtained by controlling the interior reaction temperature of the epoxy resin. Second, the sample having optimal electrical and mechanical characteristics is obtained for the repetitive post-curing method at 100c in view point of the post-curing conditions of the epoxy resin. Third, it appears that tan and characteristics at LN2 temperature are about half of those at room temperature. Fourth, it appears that the dielectric strength of the epoxy resin at LN2 temperature is higher by about 0.6-1.0 MV/cm than that at room temperature. The heat-aging of the epoxy resin due to the micro-defect and excess fever-movement have been noticed to affect dielectric strength at LN2 temperature more significantly than at room temperature.

• Journal of Plant Biotechnology
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• v.34 no.3
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• pp.263-269
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• 2007

To establish a optimum culture condition in vitro for production of seedlings in Wasabia japonica, the effects of salt strength, sucrose concentration, and $NH_4/NO_3$ ratio on the shoot growth in MS medium were investigated. The full strength of MS medium was the best condition for shoot growth, and in $1/4{\sim}1/2x$ or 2x MS medium the growth was significantly suppressed. Growth of shoots was enhanced when sucrose was added in MS medium after 2 weeks of culture, and the best result was found at 3% sucrose addition. ${NH_4}^+/{NO_3}^-$ ratio of 10:50 gave the highest biomass of shoot in the liquid culture with MS medium, and increasing the ${NH_4}^+$ ratio in the medium significantly reduced the growth of shoot.

• Transactions of the Korean hydrogen and new energy society
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• v.34 no.5
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• pp.526-534
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• 2023

To evaluate the risk of leakage when using liquid hydrogen, a leakage test was conducted using liquid nitrogen in an outdoor environment rather than a laboratory environment. To assume a real-scale continuous leak, liquid nitrogen was allowed to leak for 5 minutes through a pipe with a diameter of 25.4 mm at a design spill rate of 60 L/min. The measurement system consisted of devices for climate conditions, LN2 spread and vapor clouds. The main experimental results are the liquid pool radius and the concentration of vapor cloud, and the radius of the liquid pool was compared with the numerical analysis results.

• Aerospace Engineering and Technology
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• v.7 no.2
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• pp.170-175
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• 2008

In this study, it was investigated that the characteristics of startup and compatibility using several type hot and cold gases. The characteristics of starting LRE by pyro starter was compared with that by a Helium spinner. The compatibility of pyro gas, a gaseous Helium, Hydrogen+Nitrogen mixture gas, and air was investigated by a simple 1D turbine analysis considered the properties of each gas and turbine efficiency. Most of them were compatible to start up the LRE however air was properly used only for low power mode of turbine.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.90-90
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• 2003

한국항공우주연구원은 액체추진기관 시스템을 이용한 3단형과학로켓(이하 KSR-III)을 국내 최초로 개발하여 비행시험을 수행하였다. 액체추진기관 로켓의 비행시험을 위해서는 이전의 고체 추진기관을 이용한 과학로켓 1, 2와는 달리 비행시험 조건에 부합하게 액체추진제 및 가압제 등을 공급하는 지상설비가 필요하다. 이에 한국항공우주연구원은 독자적으로 비행시험에 필요한 제반 설비를 갖춘 발사장을 구축하였다. KSR-III는 압축 헬륨가스(GHe)를 이용하여 연료(Jet A-1)와 산화제(LOx)를 가압하여 추력을 얻는 액체추진기관 시스템이다. 따라서 발사장에서의 지상공급설비는 유공압 설비와 발사시나리오에 따라 해당 부품을 제어하고 자료를 저장하는 제어/계측 설비 및 기타설비들로 구성되어 있다. 지상공급설비 중 유공압 설비는 LOx의 저장 및 기체 내 산화제 탱크의 충전을 위한 산화제 공급설비, Jet A-1의 저장 및 기체 내 연료 탱크의 충전을 위한 연료 공급 설비, 지상설비용 밸브구동 및 기체 내부 퍼지 등에 필요한 질소($N_2$)를 저장/공급하는 설비, 기체내부 밸브 구동 및 가압제로 사용되는 기체헬륨(He)을 저장/공급하는 설비들로 구성되어 있다. 이러한 구축된 공급설비는 기능시험, 연계시험 등의 각종 입증시험을 통해 그 성능을 검증한 후 단인증모델(SQTM)을 이용하여 발사 시나리오에 따른 추진제 공급능력을 입증한 후 KSR-III의 비행시험을 성공적으로 수행하였다. 수행된 연구결과는 향후 건설되어질 우주센터내의 발사장 기반설비 설계의 기초 자료로 활용할 수 있을 것이다.

• Journal of Korean Society of Forest Science
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• v.97 no.3
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• pp.285-290
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• 2008

This study was carried out to obtain an optimal liquid culture condition for Sarcodon aspratus mycelia. Among various basal culture media the GYS (glucoe-yeast extract-soytone) medium was the best for mycelial growth. The appropriate temperature was $25^{\circ}C$. Starch, maltose or glucose was excellent carbon sources for the mycelial culture, compared to others tested. As nitrogen nutrients, soytone and $NH_4-N$ were the best organic and inorganic nitrogen sources, respectively. Moreover, the optimal concentration of soytone was 3 g per one-liter medium. In addition, we also found that alanine, $(NH_4)H_2PO_4$, and nicotinic acid were the best aminoacid, phosphorus salt, and vitamin, respectively. When all optimal conditions described above were applied to culture medium, we were able to produce 5.7 g dry weight of S. aspratus mycelia per one-liter liquid medium within 20 days.

• Proceedings of the KIEE Conference
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• 2001.11a
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• pp.234-237
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• 2001

고온초전도 기기의 냉매로 사용되는 액체질소($LN_2$)의 절연파괴 특성을 평가하고 기존 변압기에 사용되는 변압기유의 절연파괴 특성에 대하여 비교하였다. ��치에 따른 기포발생을 모의하여 순수 액체와 기포가 포함된 액체의 절연내력을 평가하였으며 기포의 거동에 따른 절연내력을 고찰하였다. 또한, 고온초전도 변압기, 케이블 및 한류기 등은 괜치 발생위치가 명확하지 않으므로 기포의 발생위치를 세 부분으로 모의하여 절연파괴 특성을 고찰하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.4-4
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• 2000

KSR-III 과학로켓 개발사업의 한 분야인 추진기관 연구에 있어 가장 중심이 되는 것은 제작된 연소실의 시험/검증이라고 할 수 있다. 여러 단계의 시험 가운데에서도 엔진의 특성을 제 1차 적으로 파악하고, 시험 대상물인 엔진을 스탠드에 장착하여 시험이 가능토록 하기 위해서 모사 추진제(물) 혹은 실제 추진제를 사용하여 수력학적 특성을 알아내는 것은 매우 중요하다. 이를 위해 engineering model 엔진(이하 EM)에 대하여 액체 산소 배관은 액체 산소를, 스탠드 사정상 케로신 배관은 액체 질소를 사용한 비연소 시험을 수행하였으며, 이러한 일련의 비연소 시험을 통해 산화제 및 연료 매니폴드 각각에 대한 차압과 매니폴드를 채우는 시간을 측정하여 점화 사이클을 정의할 수 있었다.(중략)