• Title/Summary/Keyword: 융삭

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Study on the Nozzle Surface Regression Mechanism (노즐 표면 삭마 미케니즘에 대한 고찰)

  • Lee Tae-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.141-143
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    • 2006
  • It is well known that there are three mechanisms in the nozzle surface regression, namely ablation, mechanical erosion and chemical corrosion. There are Analogies among these three mechanisms. In order to compare the order of the magnitude of these mechanism, the analogy was adapted and the Mach number of the gas flow was expressed by the nozzle shape(location).

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Research on Applicability of Laser Ablation Propulsion to Space Debris Removal by Simulations (시뮬레이션을 통한 레이저 융삭 추진의 우주 쓰레기 제거 응용 가능성 연구)

  • Yoo, Seong-Moon;Lee, Seung-Min
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.2
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    • pp.169-176
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    • 2022
  • Laser ablation propulsion(LAP) is the method to create impulse by laser ablation. It can be used to deorbit the space debris(SD), as its long-range property and versatility on any material. In this paper, we find out several requirements of the LAP system(LAPS) to deorbit the SD by simple numerical calculations of the SD orbit and laser beam flux. As a result, minimum operable altitude angle turned out to be a crucial variable to the LAPS. Moreover, if minimum operable altitude angle is 10°, and if the minimum distance between the LAPS and the SD is below 450 km, 1 m/s2 is sufficient to deorbit the SD by once. With 18 kJ/3 ns pulsed laser and cube shaped 100 kg SD, 1 m/s2 acceleration can be achieved by increasing the pulse repetition rate over 34~53 Hz, depending on the size of the SD. This capability could compare with the conceptual design of the Japan Establishment for a Power-laser Community Harvest(J-EPoCH) facility, which include 8 kJ, 5 PW@100 Hz laser.

$CF_4$ abatement technique with 3 phase AC plasma torch (삼상 교류 플라즈마 토치를 이용한 $CF_4$분해기술)

  • Lee, K.H.;Kim, K.S.;Lee, H.S.;Lim, G.H.
    • Proceedings of the KIEE Conference
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    • 2002.07c
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    • pp.1820-1822
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    • 2002
  • 본 논문에서는 반도체 제조공정에서 발생하는 $CF_4$의 분해와 제거를 위하여 3상 교류 플라즈마 토치를 제작하고, 플라즈마를 발생시켜 $CF_4$제거 가능성과 이에 따른 문제점에 대해 알아보았다. 매우 강하고 안정한 C-F 결합을 깨고 $CF_4$가스를 분해하기 위해서는 1100[$^{\circ}C$]정도의 고온이 필요한데, 본 실험의 플라즈마 플레임의 경우 $CF_4$가스를 열분해 광분해 시키기에는 충분한 온도와 에너지를 가지고 있다고 사료된다. 하지만 고온의 플라즈마와 토치 내부의 복잡한 유동과 고온의 플라즈마에 의한 전극의 융삭문제는 플라즈마를 연속적으로 발생시켜 $CF_4$가스의 제거효율을 높이기 위해서는 필히 개선해야 할 문제점인 것으로 사료된다.

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