• Title/Summary/Keyword: 공대사

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Biodegradation Study of Gasoline Oxygenates by Butane-Utilizing Microorganisms (부탄 분해 미생물을 이용한 휘발유 첨가제의 분해특성)

  • 장순웅
    • Journal of Soil and Groundwater Environment
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    • v.8 no.1
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    • pp.27-34
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    • 2003
  • In this study, potential degradation of MTBE and other gasoline oxygenates by pure culture ENV425 and mixed culture isolated from gasoline contaminated soil using butane as the sources of carbon and energy was examined and compared. Butane monooxygenases(BMO) of butane-grown ENV425 and mixed culture generated 1-butanol as a major metabolite of butane oxidation and addition of acetylene, specific inhibitor of monooxygenase, inhibited both butane oxidation and 1-butanol production. The results described in this study suggest that alkanes including propane, pentane, and butane are effectively utilized as a growth substrate to oxidize MTBE cometabolically. And also BTEX compounds could be the potential substrate of the MTBE cometabolism. Cell density also affected on the MTBE degradation and transformation capacity(Tc). Increasing cell density caused increasing MTBE degradation but decreased transformation capacity. Other result demonstrated that MTBE and other gasoline oxygenates, ETBE and TAME, were degraded by butane-grown microorganism.

회원작품

  • Korea Institute of Registered Architects
    • Korean Architects
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    • no.11 s.188
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    • pp.5-22
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    • 1984
  • PDF

회원작품

  • Korea Institute of Registered Architects
    • Korean Architects
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    • no.6 s.219
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    • pp.7-23
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    • 1987
  • PDF

Computation Algorithm for Launch Acceptability Region of Air-to-Surface Missiles (공대지 유도탄의 발사유효범위(LAR) 산출 알고리듬)

  • Park, Sang-Sup;Hong, Ju-Hyeon;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.10
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    • pp.910-919
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    • 2015
  • A weapon control algorithm equipped on a fighter is closely related to the mission accomplishment and fighter survivability during the engagement. In the case of a air-to-surface missile, the weapon control algorithm typically provides a pilot the target shoot-down possible region known as launch acceptability region(LAR) in the multi function display(MFD). LAR is produced by the range table(RT) through computation of an engagement range. In this paper, the operation system of AGM-84 and AGM-88 air-to-surface missiles is introduced. And the engagement range computation and LAR algorithm based on the real-time pseudo 6-DOF simulation are proposed. In order to verify the performance of the algorithm, numerical engagement simulations of air-to-surface missiles to produce LAR have been done.