• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.9
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• pp.5763-5768
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• 2015

A relief valve is a mechanical element to keep safety by controlling high pressure. Usually, the high pressure is relieved by using the spring force and letting the fluid to flow from another way out of system. When its normal pressure is reached, the relief valve can return to initial state. The relief valve should be designed for smooth operation and should satisfy the structural safety requirement under operating condition. The commercial software ANSYS/WORKBENCH is utilized for flow and structural analysis. Very high pressure may cause structural problem due to severe stress. The study suggests the design satisfying the structural design requirement

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.3
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• pp.258-263
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• 2012

In this paper the Chemical Propulsion Subsystem of COMS is briefly explained and some telemetries acquired by a series operations of CPS during the Launch and Early Operation Phase of COMS are presented. The pressure and temperature of pressurant tank telemetries are compared with the results of the developed computer program. The changes in pressure are due to the two major phases. The first one is the initialization phases of CPS composed of the venting phase to vent the helium gas in the pipe network from the downstream of the propellant tanks to the thrusters for safety, the priming phase to fill the vented pipe network with oxidizer and fuel respectively and then the pressurization phase to pressurize the ullage of propellant tank to regulated pressure. And the other is the apogee engine firings in which COMS CPS is in the orbit raising phase to use helium as a pressurant to keep the pressure of propellant tank as the liquid apogee engine get fired until COMS reached to the target orbit. This program can be applicable to prepare basis design data of the next Geostationary Satellite CPS.

• Journal of the Korean Ceramic Society
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• v.42 no.1
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• pp.22-27
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• 2005

The preparation of B4C by SHS in $B_{2}O_{3}-Mg-C$ system was investigated in this study. In the preparation of B4C, the effect on reactivity and reaction products of the initial pressure of inert gas in reactor, the content of Mg and C in mixture was investigated. The minimum initial pressure of inert gas in reactor for SHS reaction in this system was 25 atm, and as the pressure increased, the concentration of unreacted Mg decreased and combustion temperature increased. At the initial inert gas pressure in reactor of 25 atm, the optimum composition for the preparation of pure B4C was $2B_{2}O_{3}+6.3Mg +0.94C$. The B4C synthesized in this condition had an irregular shape and the particle size of $1\~3{\mu}m$.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.5
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• pp.385-390
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• 2015

The flow characteristics in micro shock tube are investigated experimentally. Studies were carried out using a stainless steel micro shock tube. Shock and expansion wave was measured using 8 pressure sensors. The initial pressure ratio was varied from 4.3 to 30.5, and the diameter of tube was also changed from 3mm to 6mm. Diaphragm conditions were varied using two types of diaphragms. The results obtained show that the shock strength in the tube becomes stronger for an increase in the initial pressure ratio and diameter of tube. For the thinner diaphragm, the highest shock strength was found among varied diaphragm condition. Shock attenuation was highly influenced by the diameter of tube.

• Nuclear Engineering and Technology
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• v.25 no.3
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• pp.413-423
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• 1993

This paper reports an experimental study of direct containment heating (DCH) which would occur if the primary system pressure is still high at the time of vessel breach during a light water reactor core melt accident. The experiments were conducted in 1/30-scale cavity models of Kori unit 1 and 2 and Young Kwang unit 3 and 4 nuclear power plants. One 1/20-scale model of the Kori plant was also used to investigate the scaling effect. The primary variables in the experiments were initial vessel pressure, vessel breach size and cavity geometry. It is observed that higher initial pressure and larger breach size enhance the melt dispersal fraction. Also, the cavity geometry appears to affect the dispersal rate greatly. A simple correlation of melt dispersal fraction is proposed in terms of nondimensional effective period. This correlation shows good agreement with the present experimental data, the KAIST data and the BNL data.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.8
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• pp.744-749
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• 2011

In this study, determination method of initial optimal nozzle expansion in pintle rocket was investigated. The initial optimal initial nozzle expansion was decided by maximizing the mass-averaged thrust coefficient that is calculated from thrust coefficient of minimum and maximum chamber pressure. The determination of initial optimal initial nozzle expansion was equivalent to that of the minimum propellant mass which was required for obtaining the desired mission performance. The highest pressure, thrust turndown ratio and total impulse ratio effected on the initial optimal nozzle expansion. Among them, total impulse ratio had great influence on the initial optimal nozzle expansion.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1115-1121
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• 2017

In order to obtain high thrust at the beginning of the flight, the solid rocket motor with large initial burning surface area was designed and tested. From the static firing test, lower initial thrust was obtained compared with the expected thrust based on the internal ballistic prediction due to the negative erosive burning effect which reduced the burning rate estimated by APN Law. In addition, the radial mode combustion instability was observed with 8 fins grain configuration. This instability was removed after the odd number of fins were used.

• Korean Journal of Materials Research
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• v.1 no.4
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• pp.177-183
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• 1991

Change of the properties of selective CVD-W by $SiH_4$ reduction with the variation of deposition time and pressure has been investigated. The lime required for covering the who)to Si substrate by tungsten at $300^{\circ}C$ under the pressure of 100mtorr is approximately 30 seconds. The film thickness tends to increase linearly in the early stage of deposition process and parabolically later, sheer resistance of the film tends to decrease rapidly initially, and slowly later with deposition time. Tungsten grain size does not change much, but grain boundary becomes hazy in the pressure range of 50-300mtorr. Also no ${\beta}-W$ but only ${\alpha}-W$ was found in this pressure range. The deposition rate and electrical resistivity of tungsten tend to increase wish increasing pressure. The results of AES analysis show that pressure does not much affect Si/W ratio of the tungsten film and silicidation at the W/Si interface.

• Journal of the Korean Society of Clothing and Textiles
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• v.13 no.2 s.30
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• pp.117-127
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• 1989

여성 파운데이션용 편포의 압력특성에 관한 문제를 공학적 관점에서 검토해보기 위하여 거들용 편포와, 또한 비교를 위하여 드로우어즈용 편포를 시료로하여 완전강체 및 완전탄성체, 그리고 강체와 탄성체를 동시에 가지는 수압체를 모델로 제작하고, 시료를 고리형태로 만들어 피복시킨후 그 압력을 12시간 동안 연속측정하였다. 이때 시료의 신장정도, 수압체의 탄성체 구성비 등을 여러가지로 달리 하여 그에 따른 압력의 변화를 봄과 동시에 시간경과의 효과도 검토하여본 바 다음과 같은 결과를 얻었다. 1. 강체를 수압체로한 경우는 시료의 신장률 증가에 따라 압력이 거의 직선적으로 증가하였고, 그 정도는 거들의 재료가 드로우어즈의 재료에 비하여 훨신 크게 나타났다. 2. 수압체의 탄성체구성비가 증가할수록 신장률 증가에 따른 시료의 실질신장률의 증가 경향이 둔화되어, $40\%$신장률의 경우는 그 이전보다 오히려 감소하는 경향을 나타내었다. 3. 수압체에 탄성체가 포함된 경우는 매우 적은 압력을 나타내었으며, 시료 신장률의 증가에 따른 변화도 매우 적게 나타남으로써 시료 신장률이 클수록 강체수압체에 대한 압력과의 차이가 더욱 커지게 됨을 알 수 있었다. 그러나드로우어즈 재료의 경우는 탄성체가 받는 부담은 크지 않은 것으로 나타났다. 4. 압력의 경시변화는 초기의 압력분포 안정화 과정을 제외하고는 12시간까지 어떤 경우에도 크게 나타나지 않았다.

• Journal of the Korea Concrete Institute
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• v.24 no.5
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• pp.605-612
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• 2012

Spalling of concrete occurs due to vapor pressure ignited explosion, temperature difference across a section, and combination of these factors. Factors affecting spalling can be classified into internal and external factors such as material property and environmental condition, respectively, have to be considered to precisely understand spalling behavior. An external environmental factor such as differences in heating rate cause internal humidity cohesion and different vapor pressure behavior. Therefore, spalling property, vapor pressure and thermal strain property were measured from concrete with compressive strengths of 30 MPa, 50 MPa, 70 MPa, 90 MPa, and 110 MPa, applied with ISO-834 standard heating curve of $1^{\circ}C/min$ heating rate. The experimental results showed that spalling occurred when rapid heating condition was applied. Also, when concrete strength was higher, the more cross section loss from spalling occurred. Also, spalling property is influenced by first pressure cancellation effect of thermal expansion caused by vapor pressure and heating rates.