• 한국전산유체공학회:학술대회논문집
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• 2008.03b
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• pp.324-327
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• 2008

Two stage startup of high thrust liquid rocket engine can reduce the abrupt impulse to the vehicle and engine by changing oxidizer flow rate to the combustion chamber. Also it ensures stable ignition of combustion chamber against hard start and to prevent pump stall by the sudden supply of large mass flow rate. However high discharge pressure of oxidizer pump or temperature rise in gas generator may be a problem in applying the preliminary stage. To solve this problem, we analyzed the effect of the slope of oxidizer pump's head curve and the oxidizer mass flow rate to combustion chamber during preliminary stage using the rocket engine startup analysis code. A moderate slope(${\circleddash}{\sim}$-3) of head curve and 80% mass flow rate during preliminary stage can reduce the oxidizer pump discharge pressure by 15 to 20% comparing with the condition of ${\circleddash}$=-4.37 head curve and 70% mass flow rate. Also it can maintain the turbine inlet temperature rise within 50K from the nominal value.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.3
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• pp.26-33
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• 2014

The gas-centerd swirl injectors are widely used on the main combustor of large liquid propellant rocket engines. Since the gas-liquid propellants, such as kerosene and oxygen-rich gas combination, are mixed and burned in the high pressure condition over the critical pressure point, the cold-flow spray test in the atmospheric condition can not represent the actual spray pattern. To observe the near actual spray patterns of gas-centered swirl injector, the high pressure spray chamber and the control system were constructed. The operating sequence was controlled precisely to obtain clear visualization images.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.443-446
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• 2012

A thrust control valve of a liquid rocket engine plays a role to increase or decrease the thrust of an LRE by modulating the flow rate of propellant into a gas-generator. This paper deals with a flow regulator that has functions of not only modulating thrust but also maintaining constant flow rate regardless of pressure change at inlet or outlet of the flow regulator. A direct acting flow regulator was fabricated and tested for the comparison of experimental and simulation results under steady-state conditions. The drawbacks and limitations of the flow regulator were analyzed. Also the new design of a flow regulator was proposed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.484-488
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• 2012

Korea Aerospace Research Institute (KARI) performed the conceptual design of rocket engine test facility for the development and qualification of the 3rd stage liquid rocket engine for KSLV-II. The 3rd stage rocket engine test facility, which are to be constructed at Naro Space Center, will supply propellants and high-pressure gases to engine for firing test at ground and altitude conditions. The altitude test condition is obtained using a supersonic diffuser operated by the self-ejecting jet from the liquid rocket engine.

• Nuclear Engineering and Technology
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• v.17 no.1
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• pp.45-52
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• 1985

A two inverted U-tubes condenser was constructed from transparent materials to study the heat removal capability of steam generators under filmwise reflux condensation mode. Essentially, two sets of experiments were performed: (1) the first dealt with the reflux condensation length, and (2) the second dealt with the flooding points with and without the presence of a noncondensible gas in the steam flow, and the effect of the flooding time. In addition, experimental results are compared with the predictions of analytical models.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.10
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• pp.966-978
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• 2011

Transpiration cooling is the most effective cooling technique for the high-performance liquid rockets and air-breathing engines operating in aggressive environments with higher pressures and temperatures. When applying transpiration cooling, combustor liners and turbine blades/vanes are cooled by the coolant(air or fuel) passing through their porous walls and also the exit coolant acting as an insulating film. Practical implementation of the cooling technique has been hampered by the limitations of available porous materials. But advances in metal-joining techniques have led to the development of multi-laminate porous structures such as Lamilloy$^{(R)}$ fabricated from several diffusion-bonded, etched metal thin sheets. And also with the availability of lightweight, ceramic matrix composites(CMC), transpiration cooling now seems to be a promising technique for high-performance engine cooling. This paper reviews recent research activities of transpiration cooling and its applications to gas turbines, liquid rockets, and the engines for hypersonic vehicles.

• Resources Recycling
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• v.15 no.1 s.69
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• pp.12-19
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• 2006

Rice straw is one or the main renewable energy sources in Korea. Bio-oil is produced from rice straw with a lab-scale equipment mainly with a fluidized bed and a char removal system. It was investigated how the reaction temperature affected the production of bio-oil and the efficiency of a char removal system. To elucidate how the temperature depended on the production of bio-oil, experiments were conducted at $466^{\circ}C,\;504^{\circ}C\;and\;579^{\circ}C$, respectively. The mass balance was established in each experiment, and the produced gas and oil were analyzed with the aid of GCs and a GC-MS system. The char removal system is composed of a cyclone and a hot filter. Tn the experiments, we observed that the production of bio-oil was decreased with temperature, and the bio-oil contained very useful chemicals.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.12
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• pp.109-116
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• 2005

Elastic-plastic structural analysis for regenerative cooling chamber of liquid rocket thrust chamber is performed. Uniaxial tension test is also conducted for the copper alloy in order to get material data necessary for the structure analysis. The results of uniaxial tension test reveal that copper alloy become ductile after brazing process and flow stress becomes lower as temperature becomes higher. As a result of structural analysis using the material data, the deformation of cooling channel is more increased by thermal load than by internal pressure of cooling fluid. Therefore, the results of analysis show that structural stability and cooling performance of combustion thrust chamber which is designed to endure mechanical load and minimized a channel thickness are improved by decreased thermal load as possible.

• Korean Chemical Engineering Research
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• v.47 no.4
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• pp.446-452
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• 2009

The behavior of a one-step fixed bed reactor which directly synthesizes dimethyl ether(DME) from Natural Gas was simulated. In the reactor, the prevention of the occurrence of hot spots which can cause deactivation of catalysts is pivotal, since methanol synthesis and dehydration reaction involved in the synthesis of DME are highly exothermic. Therefore, we simulated and compared performance of the reactor with counter-current cooling and pool boiling system that can be applied to a commercial plant. As a result, we found that counter-current cooling system is more effective in terms of CO conversion and DME productivity. However, pool boiling system can operate in a small temperature gradient that can decrease problems caused by hot spot. And, the system can operate in a safer range.

• Proceedings of the Korean Society of Embryo Transfer Conference
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• 2002.11a
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• pp.93-93
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• 2002

싸움소(투우)는 1999년 문화관광부지정‘한국의 10대 지역문화 관광축제’로 선정되어, 청도군 투우대회가 한국을 대표하는 축제가 되었고, 상설투우장의 건설로 새로운 레져 산업으로 부상하고 있다. 그러나 싸움소 생산에 소요되는 유전인자 보존 및 생산기반은 전무한 실증이며, 본 연구는 청도군내 우수 종모우을 선별하여 정액채취 및 동결정액을 생산하여 군내 한우번식 농가에서 인공수정을 실시하고 계절별 수태율과 송아지의 성비를 조사하였다. 종모우 번개(나이6세, 체중850kg, 97, 98년 우승)와 사자(나이6세, 체중870kg 98, 99년 준우승) 2두로부터 일반적인 방법으로 인공질을 이용하여 1999년 10월에 정액을 채취하였다. 채취된 정액은 35$^{\circ}C$에서 3~5배정도로 희석하여 정자농도와 활력을 평가하였다. 희석정액은 90분간에 걸처 5$^{\circ}C$ 까지 냉각하면서 글리세롤을 첨가한 난황구염산나트륨액으로 여러번 나누어 희석하여 정자의 충격을 피하였다. 글리세롤평형 2시간 후 0.5$m\ell$스트로에 정자수가 3500만/스트로의 분주.봉인하여, 정액의 동결은 액체질소상에서 4~5cm 위에 스트로를 평행으로 놓아 액체질소 가스로 10~15분간 예비동결한 다음, -8$0^{\circ}C$의 초저온 냉장고에서 케니스터에 넣어 -196$^{\circ}C$ 액체질소에 보관하였다. 인공수정을 실시하고 40일 전후에 직장검사를 통해 임신율과 수태율을 조사하고 분만한 송아지의 성비를 기록하였다. 채취한 싸움소의 정액량은 번개와 사자가 각각 평균 4.6$m\ell$와 3.8$m\ell$이고, 동결전의 정자의 활력은 번개와 사자의 정액이 각각 70.3 vs 75.3%, 동결후의 활력은 37.3 vs 40.3%로 유의한 차이는 없었다. 번개와 사자의 동결정액으로 각각 44두와 127두를 인공 수정하였고, 40일 전후의 임신율은 26두 vs 80두(59.1 vs 63.0% )였으며, 수태율은 26두 vs 66두(59.1 vs 52.0% )로 이들간의 유의한 차이는 없었다. 번개와 사자의 수송아지의 성비는 각각 65.3 vs 42.4%로 유의한 차이가 있었다. 싸움소 정액 동결보존과 인공수정으로 싸움소 혈통을 가진 송아지가 생산되었다. 그러나 생산된 송아지가 싸움소의 능력을 가진 것을 선별하여 혈통을 고정시키고, 훈련으로 싸움소의 제질을 발굴하는 것이 앞으로의 연구과제이다.