• Title/Summary/Keyword: 시험 구간 개폐밸브

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The Development of Straddle Packer Hydraulic Testing Equipment to Characterize Permeability in Deep Boreholes (장심도 시추공 정밀수리시험 장비 구축)

  • Kim, Kyung-Su;Park, Kyung-Woo;Ji, Sung-Hoon
    • The Journal of Engineering Geology
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    • v.20 no.2
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    • pp.213-220
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    • 2010
  • The permeability characterization on the natural barrier for deep geological disposal of radioactive waste is very critical to evaluate total safety and performance assessment of disposal site. However, the confidence level in using previous hydraulic testing equipments consist of simple components to estimate rock mass permeability is not high enough to reflect in situ condition. The purpose of this research is to establish an advanced hydraulic testing equipment, which is applicable to deep borehole (up to 1,000 m), through the improvement of technical problems of previous packer systems. Especially, the straddle packer hydraulic testing equipment was designed to adopt both the hydraulic downhole shut-in valve(H-DHSIV) to minimize the wellbore storage effect and the real time data acquisition system to measure the pressure changes of test interval including its upper and lower parts. The results from this research lead to not only improve current technical level in the field of hydraulic testing but also provide important information to radioactive waste disposal technology development and site characterization project.

Manufacture & Launch of Small PE/$LN_2O$ Hybrid Rocket with 50 kgf Thrust Level (추력 50 kgf 급 PE/$LN_2O$ 소형 하이브리드 로켓 제작 및 시험발사)

  • Kim, Hyeon-Woo;Jeon, Min-Ho;Oh, Ji-Sung;Han, See-Hee;Kang, Min-Seok;Jang, Hyoung-Gui;Kim, Hee-Yong;Bae, Tae-Hyun;Lee, Sun-Jae;Kim, Jin-Kon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.507-510
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    • 2009
  • The small size of hybrid rocket using PE-$LN_2O$ was designed, constructed and launched for a development basic technology of Hybrid rocket vehicle. The hybrid engine ignition system was designed with valve system using external actuator and confirmed working without any fault. To design fuel grain an internal ballistics design was carried out, and to estimate rockets flight path an external ballistics analysis was carried out. So the rocket was designed and constructed, and the launch test proves that hybrid rocket's design was suitable. The hybrid rocket(weight : 9kg, diameter : 110 mm, height : 1.7 m) was launched successfully. But parachute was deployed on mid-flight and the mission could not finish its purposed flight. Some of problems were found in this activity but next launch vehicle will be improved.

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