• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.110-113
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• 2007

For the development of hydrazine decomposition catalyst, Hot-fire test to verify performance of catalyst is required. The purpose of a long-life firing test is to demonstrate the capability of a design to perform for the maximum duration or cycles of operation. This paper describes the progress of the catalyst performance test, explains the test matrix, and presents the test results.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.407-412
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• 2006

Most of the monopropellant thrusters use catalyst for decomposing hydrazine. The thruster lifetime is determined mainly by catalyst lifetime, which can be investigated by firing tests. For the development of hydrazine decomposition catalyst, Hot-fire test to verify long-life performance of catalyst is required. This study describes the development of test equipment for long duration hot-firing and test/evaluation plan.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.6
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• pp.68-74
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• 2014

During the life firing test of 1 N-class thruster development model, pulse mode performance and performance changes were examined. The deviation of pulse mode response time according to thruster feed pressure was relatively small and the resultant ignition delay, response time, tail-off time were 32-35 ms, 86-91 ms, 89-98 ms, respectively. For the stabilized pulse region the impulse bit revealed the outstanding reproducibility of 1.41, 1.32, 2.10% at $3{\sigma}$. During the life firing test, the impulse bit was decreased with limited amounts, therefore the pulse mode performance could be considered to be maintained. The thrust centroid was also maintained during the life firing test.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.547-548
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• 2011

본 논문에서는 한국전력공사에서 장기열화 시험을 수행한 154kV 고분자애자의 성능평가를 수행하고 그 결과를 1999년부터 2008년까지 한국전력공사154kV 송전선로에 시범 설치한 고분자애자의 주간코로나, 열화상 측정을 시행하고 제조회사/규격별 각 24련을 발취하여 총 168련에 대하여 한전 표준구매 규격에 따른 각종 시험을 수행하고 현 성능상태를 검증하였으며 이를 토대로 잔존 수명을 예측하고자 하였다. 대부분의 애자가 양호한 성능을 보이고 있으나 일부 애자에서는 부적합 결과를 보였으며 수명의 경우, 초기 품질계수 정보 부족 및 중간열화 상태의 데이터 부족으로 정확한 잔존수명 예측 데이터를 얻기에는 부족했으며 추가적인 가속열화시험 등의 데이터를 확보해야 할 것으로 사료된다.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05b
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• pp.600-605
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• 1998

체내방사능 측정시스템의 교정인자는 측정결과에 주요한 요인으로 작용한다. 교정인자는 특정 집단으로부터 표준체위와 표준장기를 도출, 이를 기초로 하여 제작한 펜텀으로부터 구하는 것이 일반적인 방법이다. 그러나 팬텀의 기하학적 구조 및 내부장기의 형상은 특정 집단에 따라 다르므로 이로 인한 측정오차가 발생할 수 있다. 따라서 본 연구에서는 북아메리카 성인남성의 표준자료에 근거하여 제작된 LLNL 팬텀과 일본성인 남성의 표준자료에 근거하여 제작된 JAERI 팬텀을 한국원자럭연구소 폐 카운터를 이용하여 상호비교.분석하였다. 이와 함께 LLNL 팬텀으로 교정된 폐 카운터의 성능시험을 JAERI 팬텀으로 DOELAP 성능시험범주 I, II, III 및 IV에 대해 수행하여 편텀의 구조 및 형상으로부터 발생하는 측정오차를 분석하였다. 비교.분석결과 1.7 cm ~ 3.7 cm 근육등가 가슴벽두께 범위내에서 JAERI 팬텀에 의한 교정인자가 전반적으로 LLNL 팬텀의 것보다 다소 높은 수치를 보였으나 허용수준이었고, 성능시험결과 상대편중은 DOELAP 성능 용인 기준을 만족하였다. 결국 두 팬텀간의 측정오차는 측정 및 체내피폭선량 평가시 수반되는 오차와 비교해 보면 그다지 크지 않은 것으로 결론지울 수 있다. 따라서 LLNL 펜텀으로부터 구한 교정인자를 국내 성인남성의 일상 모니터링에 사용할 경우 측정결과가 다소 과대평가되기는 하나 허용수준으로서 큰 문제가 없는 것으로 나타났다.

• Journal of the Society of Disaster Information
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• v.14 no.1
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• pp.79-88
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• 2018

In this study, the changes of the expansion and strength according to the temperature of the emergency repairing expansion material were examined by cup foaming test and uniaxial compressive strength test, and the accelerated compression creep test was carried out to confirm the long term stability. Ramp & Hold test and accelerated compressive creep test were performed to evaluate the creep performance. The short - term creep test was used to determine the initial creep strain of the expanding material. The isothermal method using time - To evaluate the long - term compressive creep performance.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.12
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• pp.1035-1047
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• 2015

Wind tunnel experiment and computational analysis have been carried out to evaluate the performance of propeller for scale electric-powered HALE UAV, named EAV-2H+. Performance curves are measured for three propellers and their adequacy for EAV-2H+ installation is examined through consideration of operating conditions. Decline in performance coefficients is observed in low rpm region. Also, the effect of transition tape on propeller performance is measured and analyzed. The computational performance analyses are carried out by using commercial CFD program. The thrust and power coefficient from computations show good agreement with experimental results. Performance coefficients are compared and the influence of measurement device which contributes to discrepancy of the results is examined. Transition SST model is confirmed to yield the tendency of performance decline in low rpm range, similar to experimental observation. The decrease in aerodynamic performance of blade element due to low Reynolds number is identified to cause the decline in propeller performance. Analyses for high altitude conditions confirms degradation in propeller performance.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.6
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• pp.59-67
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• 2014

Acceptance level random vibration and life firing test for development model of 1 N-class monopropellant thruster have been performed. From the results of random vibration, the natural frequency of the dual thurst module composed of 1 N-class development model thrusters was higher than the part level requirement(>100 Hz) and the structural robustness was verified. Thrust decrease of steady sate was below 7% and thrust instability was within ${\pm}5%$ in the life firing test using over 20 kg propellant throughput. The computerized tomography for catalyst bed showed a less than 7% of catalyst loss and it revealed the design appropriateness of the current thruster development model.

• Proceedings of the KIEE Conference
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• 2001.07b
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• pp.757-759
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• 2001

전동기 전원 개폐를 주목적으로 하는 전자개폐기는 빈번하고 불규칙한 개폐동작에 의해 발생되는 Arc 에너지에 대해 전기적으로 내구성능을 확보하는 것이 중요하다. 또한, 전기적 내구 성능은 수명과 품질을 결정하는 요인으로서 선진업체에서는 내구성능을 향상시키려 연구개발 활동에 집중하고 있다. 이러한 전기적 내구 성능을 향상, 평가하기 위해서는 장기간에 걸친 시험 기간과 시험규격에서 요구하는 조건을 만족시키는 시험 회로와 설비구성이 필수적이다. 여기서는 전기적 내구 성능에 대한 이해와 시험규격을 통한 시험회로 설계 및 설비제작에 대해 설명하고 시험결과를 분석하고자 한다.

• Composites Research
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• v.32 no.1
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• pp.78-84
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• 2019

This study focused on the prediction of the long-term performance of carbon fiber/epoxy composites using Dynamic Mechanical Analysis (DMA) and Time-Temperature Superposition (TTS). Single-frequency test, multi-frequency test, and creep TTS test were performed. A sinusoidal load of $20{\mu}m$ amplitude was applied while increasing the temperature from $-30^{\circ}C$ to $240^{\circ}C$ at $2^{\circ}C/min$ for the single-frequency test and the multi-frequency test. The frequencies applied to the multi-frequency test were 0.316, 1, 3.16, 10 and 31.6 Hz. In the creep TTS test, a stress of 15 MPa was applied for 10 minutes at every $10^{\circ}C$ from $-30^{\circ}C$ to $230^{\circ}C$. The glass transition temperature was determined by single-frequency test. The activation energy and the storage modulus curve for each temperature were obtained from glass transition temperature for each frequency by the multi-frequency test. The master curve for the reference temperature was obtained by applying the shift factor using the Arrhenius equation. Also, TTS test was used to obtain the creep compliance curves for each temperature and the master curve for the reference temperature by applying the shift factors using the manual shift technique. The master curve obtained through this process can be applied to predict the long-term performance of carbon fiber/epoxy composites for a given environmental condition.