• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.18 no.2
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• pp.108-115
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• 1989

과학산업의 육성책으로서 정부에서는 1988년도부터 특정출연연구 개발과제로 극한기술 개발을 시작하였다. 본 연구개발 과제는 극한기술의 5개 분과중 하나인 극저온 기술 분야에서의 연구개발목표인 SQUID(Superconductive Quantum Interference Devices)의 냉각장치로 사용되는 극저온용 냉동기 개발이다. 1988년부터 3년간, 연구개발비 약 3억원을 투자하여 작동온도 4.2K에서 약 100mW의 냉각능력을 갖는 냉동기에 대한 시제품을 개발함이 목적이다. 본 기술논문에서는 지난 6개월간의 연구수행 내용을 개략적으로 기술하여 연구진행상황을 파악할 수 있도록 하였다.

• Journal of the Korean Society for Precision Engineering
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• v.19 no.11
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• pp.31-36
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• 2002

극저온 냉동기 시장은 군수시장이 대부분이며 민수시장은 현재까지는 여러 분야에 응용되기 시작하는 시장 형성기에 있다. 그러나 향후 초전도시장과 더불어 성장이 기대되는 시장이다. 국내는 기술 개발면에서 많은 발전을 하고 있지만 아직도 외국에 비하여 뒤떨어진 실정이며 특히 극저온 냉동기의 제조 공정과 경제성 면에서의 기술발전은 본사를 제외하고서는 전무한 실정이다. 생산기술의 면에서의 연구 부족은 제한된 시장과 많은 기술장벽과 단시간의 개발기간 등에 주원인이 있다고 하겠다. 이러한 공정기술 낙후성은 가격경쟁력에서 뚜렷이 나타날 수밖에 없으며 이를 극복하기 위해서는 지속적인 개발과 체계적 지원이 뒤따라야 한다. 극저온냉동기의 국산화를 위해서는 원천기술 개발뿐만 아니라 공정 및 생산기술 개발 또한 절실히 필요하다. 따라서 많은 관계 연구자들의 연구와 관심이 뒤따라야 한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.2
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• pp.54-61
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• 2007

Propellant pressurization system in liquid rocket propulsion system plays a role supplying pressurant gas at a controlled pressure into the ullage space of propellant tanks. The most important design parameter for such propellant pressurization system is the temperature of pressurant gas fed from pressurant tank. Such pressurant is gaseous state, of which density is very sensitive to the temperature of pressurant. Generally for the propulsion system, which requires high thrust and is consisted of cryogenic propellant the pressurant is stored at high density and high pressure to reduce the weight of pressurant tanks, which are placed inside of cryogenic propellant tank. That is called cryogenic storage pressurization system. This study investigates the temperature variation of pressurant at the time when the pressurant is coming out of pressurant tank experimentally as well as numerically. Fluids used in this study are air and liquid oxygen as outer fluid and gaseous nitrogen and gaseous helium as pressurant respectively.

• Journal of ILASS-Korea
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• v.26 no.1
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• pp.18-25
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• 2021

The objective of this study is to investigate the effect of cryogenic intake air temperature on the injected fuel droplet behavior in a compression ignition engine under the different start of energizing timing. To achieve this, the intake air temperatures were changed from -18℃ to 18℃ in steps of 9℃, and the result of fuel evaporation rate, Sauter mean diameter, and equivalence ratio distributions were compared. When the intake air temperature decreased in steps of 9℃, less fuel was evaporated by about 3.33% because the cylinder temperature was decreased. In addition, the evaporated fuel amount was increased with retarding the start of energizing timing because the cylinder temperature raised. However, the difference was decreased according to the retarded start of energizing timing because the cylinder pressure was also increased at the start of fuel injection. The equivalence ratio was reduced by 5.94% with decreasing the intake air temperature. In addition, the ignition delay was expected to longer because of the deteriorated evaporation performance and the reduced cylinder pressure by the low intake air temperature.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.3
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• pp.77-81
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• 2012

In a cryogenic propellant tank the pressurant is contracted due to heat loss and the propellant itself evaporates. On a restartable propulsion system such phenomena are more intensive because the propellant contacts with the pressurant on the larger surface during the coast flight. Such heat and mass transfer phenomena should be considered for estimating the amount of pressurant. On the hypothesis that the heat and mass transfer quasi-equilibrium is achieved during the coast flight, the calculation process of the equilibrium pressure is presented. On the process the amount of loaded helium on the Falcon-1 second stage is calculated.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.21 no.2
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• pp.88-99
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• 1992

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.38 no.3
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• pp.28-34
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• 2009

LNG플랜트용 열교환기를 설계하는데 필요한 극저온 열전달의 기본 이론과 열교환기의 기본설계 기술에 대하여 소개하고자 한다.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.18 no.6
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• pp.507-514
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• 1989

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.19 no.1
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• pp.7-18
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• 1990

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.19 no.3
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• pp.175-183
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• 1990