• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.37-42
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• 2010

A design plan was proposed for determining combustor configuration of regenerative- cooled liquid rocket engine in the process of preliminary design. Rocket performance and regenerative cooling results were calculated using the properties of combustion gas estimated in CEA. For required thrust, chamber pressure, atmosphere pressure and propellant mixture ratio the mass flow rate of propellants and combustor performance were predicted using one-dimensional and experimental equations. Finally, determinable plan for contour of combustor were presented through Rao nozzle design method.

• Nuclear Engineering and Technology
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• v.15 no.4
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• pp.219-228
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• 1983

The blowdown history of the TMI-2 accident up to the isolation of the relief valve associated with a small break LOCA is reviewed briefly. An analysis is made to determine what instruments should be added in the core in order to prevent core damage in the case of the TMI-2 accident. With the added instruments a procedure is presented on how to predict the uncovered level of the core and how to calculate operator time margin. Sample calculations are done for the TMI-2 accident to determine the uncovered level and operator time margin. Finally, the map to show the uncovered level of the core and operator time margin is drawn with measurable parameters by the above methods.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.04a
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• pp.31-34
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• 2011

Design and fabrication of Technology Demonstration Model(TDM) of 75 tonf regenerative cooling thrust chamber were described. It has design chamber pressure of 60 bar, propellant mass flow rate of 243.6 kg/s, and nozzle expansion ratio of 12. It has a single welded structure of the mixing head and the chamber. Design and fabrication technologies established through this TDM can be used to development of flight model.

• Journal of the Korean Society of Clothing and Textiles
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• v.48 no.3
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• pp.501-510
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• 2024

This study aimed to compare the cooling effect of specific body parts to increase workers' thermal comfort. The parts to be cooled comprised the head and neck; the coolant was a phase change material. The participants were ten men in their 20s of average size according to the 8th Size Korea. The experiment was conducted under the following conditions: 28.0 ± 0.5℃, 60.0 ± 5.0% RH, and 0.2 ± 0.1m/s. The exercise consisted of participants moving for 15 min at a constant speed of 80 BPM; later, a subjective sensation was performed, and the clothing surface temperature was measured. In doing so, heat, wetness, and discomfort after exercise were confirmed to have increased without a coolant. Significant differences over time appeared only when no coolant was used, showing that thermal comfort decreased. Despite the addition of coolant, the clothing surface temperature gradually increased over time, but it decreased with coolant rather than without it. Therefore, additional coolant areas, a lower temperature, and simultaneous cooling convection were required to improve thermal comfort.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.1
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• pp.35-44
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• 2011

Mathematical modelling for liquid rocket engine(LRE) main components were conducted to predict the dynamic characteristics when the LRE operates at the transient condition, which include engine start up, shut down, or thrust control. Propellant feeding system is composed of fuel and oxidizer feeding components except for regenerative cooling channel for the fuel circuit. Components modeling of pump, pipe, orifice, control valve, regenerative cooling channel and injector was serially made. Hydraulic tests of scale down component were made in order to validate modelling components. The mathematical models of engine components were integrated into LRE transient simulation program in concomitant with experimental validation.

• Proceedings of the Korean Society of Embryo Transfer Conference
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• 1997.05a
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• pp.9-15
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• 1997

치밀 난구세포로 둘러싸인 소 난자를 $38^{circ}C$. 5% $CO_2$ 배양기에시 5% superovulated cow serum(SCS)이 첨가된 m-TCM 199 medium 으로 $20{\sim}22$ 시간 배양하였으며, 수정능이 획득된 정자와 체외수정하였다. 7일${\sim}$8일경의 수정란을 1.3M methyl cellosolve(MC), 1.1M diethylene glycol(DEG), 1.8M ethylene glycol(EG), 1.6M propylene glycol(PG) 및 1.1M 1,3-butylene glycol(BG) 용액에서 10분간 평형시킨 후 0.25 ml 스트로내에 장전하였다. 스트로를 $0^{\circ}C$의 alcohol bath freezer에 넣고 $-6^{\circ}C$까지 $-1^{\circ}C$/분 속도로 냉각, 식빙 후 10분간 정체시켰으며, $-0.3^{\circ}C$/분 또는 $-0.5^{\circ}C$/분으로 $-30^{\circ}C$까지 냉각 후 스트로를 액체질소에 침지하여 보관하였다. 수정란이 들어있는 스트로를 $30^{\circ}C$ 온수에서 융해하였으며, 수정란을 TCM 199 medium 으로 옮긴 후 5% SCS가 첨가된 TCM 199 medium 에서 48시간 배양하였다. 수정란이 양호한 형태를 유지하며 나중의 발육단계로 진행된 것을 생존한 것으로 간주하였다. 각 종류의 동해방지제에서 동결된 수정란의 일부는 융해 후 동해방지제를 제거하지 않고 직접 비외과적으로 이식하였다. 동결-융해 후 동해방지제의 종류에 따른 탈출배반포 발달율은 EG 50.0%, MC 53.6%, DEG 56.9%, PG 58.0% 그리고 BG 11.5%였다. $-0.3^{\circ}C$/분 또는 $-0.5^{\circ}C$/분 으로 냉각한 수정란의 생존율은 두 그룹간에 유의적인 차이가 없었으나 (P<0.05), 탈출배반포 발달율은 -0.5분 $^{\circ}C$/분(22.6%, 12/53)보다 $-0.3^{\circ}C$/분(64.6%, 31/48) 냉각시에 유의적으로 높았다(P<0.01). 동해방지제의 종류에 따른 수정란의 수태율은 MC 48%(10/21). DEG 30%(3/10), EG 74%(20/27) 및 PG 40%(4/10) 였다. 이러한 결과로 보아 MC, DEG, EG 그리고 PG는 소의 체외수정란의 동결을 위한 동해방지제로서 이용될 수 있음을 보여주었다.

• Journal of The Korean Dental Society of Anesthesiology
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• v.8 no.1
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• pp.29-34
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• 2008

배경: 신경병증성 통증은 스테로이드, 아편유사제 등의 진통제에 잘 반응하지 않는다. 하지만 염증성 매개물질들이 신경병증성 통증의 발생에 관여한다는 보고가 있다. 특히 선택적 COX2 억제제인 celecoxib의 신경병증성 통증에 대한 효과에 관해서 상반된 연구결과가 존재한다. 본 연구는 신경병증성 통증 모델인 척추신경 결찰모델을 이용 기계적, 냉각 이질통 및 온도감각 과민현상의 발현에 celecoxib이 미치는 영향을 관찰하여 celecoxib의 항통각효과를 확인하고자 하였다. 방법: 30마리의 쥐를 이용 척추신경을 결찰하여 신경병증성 통증을 유도하였다 celecoxib (1, 10, 100, and 300 mg/kg)을 경구 투여하였고 총 30마리 중 12마리의 쥐에서 열, 기계적자극에 대해서 통각과민, 냉각자극에 의해 이질통이 발생하였다. 약물 투여 후 30, 60, 120, 180분 후 von Frey, 냉각자극검사, Hargreaves검사를 시행하여 쥐의 행동변화를 관찰하였다. 결과: 신경결찰 후 5일 후에 celecoxib의 용량에 관계없이 열, 기계적 자극에 의한 통각과민, 냉각 자극에 대한 이질통을 감소시키지 않았다(P > 0.05). 또한 celecoxib투여에 의한 장기간의 항 통각효과는 관찰되지 않았다(P > 0.05). 결론: celecoxib을 경구로 투여하였을 때 장기간 유지된 신경병증성 통증 흰쥐에서 약의 투여용량, 투여기간에 따른 항 통각작용은 관찰되지 않았다. 따라서 조직 손상후 발생된 장기간의 신경병증성 통증에 있어서 celecoxib은 효과가 없는 것으로 사료된다.

• Korean Journal of Fisheries and Aquatic Sciences
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• v.31 no.4
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• pp.523-528
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• 1998

To clarify the effect of life or death condition before cooling on the physicochemical properties of plaice, Paralichthys olivaceus muscle at the early period after death, the plaices were dipped in the refrigerated sea water ($0^{\circ}C$) either as alive or after anesthesia killing. These samples were stored at $0^{\circ}C$ sea water and the changes in rigor-mortis, ATP breakdown, content of ATP and its related compounds, breaking strength and lactate accumulation through storage were investigated. Acceleration of rigor-mortis, ATP breakdown and lactate accumulation were taster in the samples refrigerated as alive than in samples killed by anesthesia before cooling. ATP in samples refrigerated as alive showed little breakdown until 7.5 hrs but it was decomposed completely after 17.5 hrs storage. The breaking strength in muscle of plaice was 1736.2 $\pm$ 65.4 g immediately after killing. The breaking strength in samples dipped in refrigerated sea water as alive increased more rapidly and showed the maximum value over 7.5 hrs (2183.3$\pm$32.2 g), However, in case of samples killed by anesthesia before cooling, the value and time reached around the maximum breaking strength were 2126.3 $\pm$ 32.2 g and 12.5 hrs, respectively and then decreased until 30 hrs. From these results, it could be suggested that dipping in refrigerated sea water after anesthesia killing before cooling is more effective in maintaining freshness of fresh plaice muscle than refrigerating as alive.

• Korean Journal of Fisheries and Aquatic Sciences
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• v.21 no.3
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• pp.177-183
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• 1988

The Present study has been carried out to investigate the effect of refrigerated seawater (RSW) at $-1^{\circ}C$ in order to delay spoilage and extend the shelf-life in Sardine(Sardinops melanosticta). The result obtained are summarized as follows : In case of freshness, K-value was shown above $30\%$ at 1 day of storage by icing, but in RSW system was shown $20\%$ until 2 days by storage. VBN and TMA were also shown the similar tendency when compared to K-value. The lipids extracted from sardine muscle held in ice was oxidized much more than those in RSW system by way of chemical test such as TBA and POV. The myofibrillar protein extracted from sardine stored in RSW system was denaturized more slowly compared with those by ice. $Ca^{2+}-ATPase$ activity indicated that myofibrillar protein held in RSW system was more stable than those held in ice. Total viable counts for sardine in RSW system showed an overall lower values. By TPA(Textural Porfile Analysis) , sardine meat pastes held in RSW system have a higher value than those held in ice.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.2
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• pp.74-80
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• 2008

The feasibility study into the development of turbine spinners, which start up the turbo-pump, has been carried out and the design requirements and parameters ranges have been presented. Turbine spinners use the solid propellant as such composite propellant based AN compound with high energy plasticizers, coolants, and phase stabilizer which relieves a sensible volume change due to the phase transformation of AN near room temperature. Propellants which have a homing rate of $0.2{\sim}0.3\;mm/s$ and pressure exponent ranged from 0.3 to 0.6, showed stable burn-out in the standard motor tests. Both the magnitude of ignition energy and its thermal transfer mechanism have been proved to have a tangible effect on the ignition of the pyre starter, and the results of this study showed that a flame temperature of 1400K would be quite adequate to get a stable ignition for the AN composite propellant.