• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.637-642
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• 2017

In this study, cold flow and combustion tests are conducted and analyzed to validate designed rocket engine head generating high temperature/pressure steam. At first, uni-injector was designed and manufactured, and cold flow test was conducted. Through this, differential pressure that can supply designed flow rate was confirmed. Also, Each injector's spray pattern were confirmed by patternator. Based on cold flow test results, we selected injectors among the candidates and arranged them on engine head, and cold flow and propellant spray tests were conducted. Finally, combustion test was carried out to analyze the flow rate, pressure, combustion efficiency. As a result, validation of rocket engine head for the development of the high temperature and high pressure steam generator has been completed.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.35 no.1
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• pp.77-84
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• 2015

Tensile tests were conducted on the GFRP reinforcement exposed to high temperature. The exposure condition for this study was below $200^{\circ}C$ for about 3 minutes. This conditioning is minor compared with that presented in experimental program conducted by other researchers. The residual tensile strength and elastic modulus of GFRP reinforcing bars at high temperature and after exposure to high temperature were compared. In results, tensile properties were decreased at high temperatures, but those after exposure to high temperature were recovered to pre-heating level almost completely. These results could be valuable for evaluating GFRP reinforced structure damaged by fire accident.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2013.05a
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• pp.140-140
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• 2013

3차원 실장을 위한 TSV의 제조 공정 중에 발생할 수 있는 Cu의 돌출 거동에 대해 연구하였다. Cu의 돌출은 반도체를 제조할 때 고온(>$350^{\circ}C$) 공정인 BEOL (back end of line) 중에 발생하는 현상이다. Cu의 돌출은 Si과 Cu의 열팽창계수 차이에 의해 발생하는 현상으로 고온 공정 뿐만아니라 열충격 시험과 같은 열피로에 의해서 발생할 수 있다. 따라서 본 연구에서는 $-65^{\circ}C$에서 15분과 $150^{\circ}C$에서 15분을 1 사이클로 설정하여 0, 250, 500, 1000 사이클의 열충격 시험을 수행하였다. 열충격 시험 후 각 사이클에서의 Cu 돌출 거동과 Cu의 표면 거칠기 변화에 대해 연구하였다.

• Journal of the KSME
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• v.49 no.5
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• pp.40-44
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• 2009

• Nuclear industry
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• v.9 no.4 s.74
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• pp.78-81
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• 1989

• Transactions of the Korean Society of Mechanical Engineers A
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• v.34 no.10
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• pp.1455-1462
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• 2010

PHE (Process Heat Exchanger) is a key component required to transfer heat energy of $950^{\circ}C$ generated in a VHTR (Very High Temperature Reactor) to the chemical reaction that yields a large quantity of hydrogen. Korea Atomic Energy Research Institute established the helium gas loop for the performance test of components, which are used in the VHTR, and they manufactured a PHE prototype to be tested in the loop. In this study, as part of the hightemperature structural-integrity evaluation of the PHE prototype, which is scheduled to be tested in the helium gas loop, we carried out high-temperature structural-analysis modeling, thermal analysis, and thermal expansion analysis of the PHE prototype. The results obtained in this study will be used to design the performance test setup for the PHE prototype.

• Proceedings of the KWS Conference
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• 2005.11a
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• pp.228-230
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• 2005

Sn-8wt%Zn-3wt%Bi (이하, Sn-8Zn-3Bi) 솔더의 장기 신뢰성을 평가하기 위하여 고용고습시험을 행하였다. 고온 고습 시험은 $85^{\circ}C$/85RH 조건에서 1000 시간 동안 하였다. 접합 기판으로는 각각 OSP (Organic Solderability Preservative), Sn 그리고 Ni/Au 처리를 한 PCB(Printed Circuit Board) 패드를 사용하였다. 접합에 사용한 부품은 1608Chip 으로 MLCC(Multi Layer Ceramic Capacitor 이하, 1608C) 와 Chip Resister(이하, 1608R)을 사용하였으며, 이 두 부품의 전극부위에 Sn-10wt%Pb(이하 Sn-l0PB), Sn을 각각 도금하였다. 솔더링 후 1608C 와 1608R의 전단 접합 강도와 솔더링부에서 Zn상의 변화를 관찰하였다. 측정결과, Sn-8Zn-3Bi 솔더의 초기 전단 접합 강도는 기판의 표면처리에 상관없이 약 40N 이었다. 그러나 고온 고습 시험 1000 시간 후에는 기판의 표면처리에 상관없이 약 30N 까지 감소하였다. 하지만 이는 reference인 Sn-37Pb 솔더의 강도값과 거의 유사하며, 이는 Sn-8Bi-3Zn 솔더의 고온 고습 시험 후 전단강도 특성은 기존 유연솔더와 비교하여 동등이상이라고 평가할 수 있다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.35 no.2
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• pp.191-200
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• 2011

A PHE (Process Heat Exchanger) is a key component of nuclear hydrogen system for massive production of hydrogen; the PHE transfers the very high temperature heat ($950^{\circ}C$) generated from the VHTR (Very High Temperature Reactor) to a chemical reaction. The Korea Atomic Energy Research Institute developed a small-scale gas loop for testing the performance of VHTR components and manufactured a modified PHE prototype for carrying out the testing in the gas loop. In this study, as a part of the evaluation of the high-temperature structural integrity of the modified PHE prototype which is scheduled to test in the gas loop, we carried out high-temperature structural analysis modeling, macroscopic thermal and structural analysis of the PHE prototype under the gas loop test conditions as a precedent study before carrying out the performance test in the gas loop. The results obtained in this study will be used to design the performance test setup for the modified PHE prototype.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.35 no.10
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• pp.1249-1255
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• 2011

A PHE (Process Heat Exchanger) is a key component required to transfer heat energy of $950^{\circ}C$ generated in a VHTR (Very High Temperature Reactor) to a chemical reaction that yields a large quantity of hydrogen. A small-scale PHE prototype made of Hastelloy-X was scheduled for testing in a small-scale gas loop at the Korea Atomic Energy Research Institute. In this study, as a part of the evaluation of the high-temperature structural integrity of the PHE prototype, high-temperature structural analysis modeling, and macroscopic thermal and elastic-plastic structural analysis of the PHE prototype were carried out under the gas-loop test conditions as a preliminary qwer123$study before carrying out the performance test in the gas loop. The results obtained in this study will be used to design the performance test setup for the modified PHE prototype.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.259-261
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• 2012

The effect of high-temperature on the flexural modulus of epoxy resin were evaluated using universal testing machine with 3-point bending and dynamic mechanical analyzer. Temperatures of $30^{\circ}C$, $100^{\circ}C$, and $140^{\circ}C$ were considered for flexural test. The specimens having aspect ratio of 16, 32, and 40 were used. The results of storage modulus from DMA were similar to those from flexural test along with given temperatures. It is found that the flexural modulus increased with increasing aspect ratio and the specimen having aspect ratio of above 32 would be suitable for the evaluation of composite material properties under high temperature condition.