• Title/Summary/Keyword: 스핀

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ESR and its Application to Magnetic Research (전자스핀공명을 이용한 자성체연구 소개)

  • Choi, Kwang-Yong
    • Journal of the Korean Magnetics Society
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    • v.20 no.3
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    • pp.120-128
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    • 2010
  • Electron spin resonance (ESR) is one of an experimental choice for studying magnetic materials that have one or more unpaired electrons. ESR spectroscopy finds its wide applications in branches of science encompassing physics, chemistry, biology, medicine and quantum computation. In this brief review we introduce a basic principle of ESR and describe how to extract information on g-factor, spin and orbital states from the ESR spectral parameters. Finally, several examples are discussed with an intention to have a practical feeling of what ESR can do in magnetism.

Fabrication and Properties of Magnetic-Tunneling Transistor Films (자기터널링 트랜지스터 박막의 제작 및 특성 연구)

  • 윤태호;윤문성;이상석;황도근
    • Proceedings of the Korean Magnestics Society Conference
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    • 2002.12a
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    • pp.172-173
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    • 2002
  • 스핀전자소자 연구 분야의 가장 큰 관심은 전하와 스핀의 자유도를 동시에 고려하여 메모리 및 논리용 트랜지스터를 구현하려는데 있다. 스핀 분극 된 전자를 자성금속으로부터 상자성 및 절연체를 이용하여 또 다른 자성체 및 반도체, 초전도체에 주입하는 일 (Spin injection)에 관한 연구가 일부 진행되어 왔다. 두 개의 자성 금속 사이에 Au등의 상자성 금속을 끼워 넣는 구조로 한쪽의 자성금속을 스핀 소스로 사용하여 상자성 금속에 스핀을 주입하고 다른 쪽의 자성금속으로 주입된 스핀을 검출하는 스핀 스위치 저장소자로서의 양극 스핀 트랜지스터 (bipolar spin transistor)를 많은 연구소에서 제조 연구하였다. (중략)

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FLIGHT TEST METHOD (SPIN) (비행시험 기법(스 핀))

  • Na, Seung-Hyuk;Lee, Ju-Ha
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.2
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    • pp.23-45
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    • 1994
  • 본 연구 논문은 항공기 개발에 있어서 비행시험의 최종 단계라 할 수 있는 스핀시험의 정의, 스핀 시험방법 및 스핀 진입시의 회복방법과 실제 비행에서의 스핀 특성으로 스핀에 대한 안전성 제고 및 비행시험의 중요성을 논하였다.

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The investigation of plastic spin behavior of body centered polycrystal with simplified accommodatio model (정적 결정수용모델에 의한 체심입방격자 다결정의 소성스핀 거동에 관한 연구)

  • Nam, Y. Y.
    • Journal of Ocean Engineering and Technology
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    • v.10 no.2
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    • pp.42-52
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    • 1996
  • 소성스핀을 취급하기 위한 이론을 살펴보면 개념적으로 현저히 다른 세가지로 압축된다. 또한 재료직조 현상이 소성스핀의 근원이라고 알려져 있지만, 그 지배인자와 발생근원에 대하여 아직 충분히 연구되어 있지 않다. 따라서 앞으로의 연구에 올바른 방향을 제시하기 위하여 소성스핀의 기본적인 거동에 대한 연구가 요구된다. 본 연구에서는 체심입방격자 다결정의 소성스핀 시뮬레이션을 통하여, 소성스핀의 거동을 조사하였는데, 재료직조, 변형경화, 변형속도, 하중역전 등의 영향을 검토하였다. 소성발생원인으로 재료직조현상이 강조되었고, 이에 관련한 주요지배인자를 제시하였다. 무차원 소성스핀은 변형속도, 재료경화에 영향을 받으나 재료직조와 관련한 인자와 비교하여 그 영향이 작게 나타났다.

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Temperature-Dependent Spin Densities in a-Ge : H (a-Ge:H에서의 스핀밀도의 온도의존성)

  • 이정근
    • Journal of the Korean Vacuum Society
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    • v.3 no.2
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    • pp.234-238
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    • 1994
  • 전자스핀 공명(ESR)으로 측정된 수소화된 비정질 게르마늄(a-Ge:H)의 D-센터에 대한 스핀밀도 의 온도의존성이 77∼350K의 온도범위에서 보고된다. a-Ge:H의 D-센터에 대하여 이 온도범위에서 온 도가 증가함에 따라스핀밀도의 감소가 관측되었으며, 그 결과는 전자상관에너지와 열적이온화효과에 근 거하는 결함 모델들의 예상치와 비교되었다. a-Ge:H에서의 스핀밀도의 감소는 전자상관에너지 모델로서 는 이해될수 없었고 상온에서의 결함계의 열적 이온화에 기인할 수 있는 것으로 생각된다.

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Study on a Spin Stabilization Technique Using a Spin Table (스핀테이블을 이용한 스핀안정화 기법 연구)

  • Kim, Dae-Yeon;Suh, Jong-Eun;Han, Jae-Hung;Seo, Sang-Hyeon;Kim, Kwang-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.5
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    • pp.419-426
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    • 2018
  • For an orbit transfer in a space exploration mission, a solid or liquid rocket booster is included at the last stage of the launch vehicle. During the orbit transfer, thrust misalignment can cause a severe orbit error. Three axis attitude control or spin stabilization can be implemented to minimize the error. Spin stabilization technique has advantages in structural simplicity and lightness. One of ways to apply the spin stabilization to the payload is to include a spin table system in the launch vehicle. In this paper, effect of the spin table system on separation dynamics of the payload is analyzed. Simple model of the spin table to mimic basic functions is designed and simulation environment is established with the model. Effect of the spin table is tested by evaluating separation dynamics of a payload with and without the spin table. Analysis on tolerance effect of separation spring constant on separation dynamics of a payload is conducted.

A Study on Dynamic Characteristics Analysis of Spindle Unit for Two-for-One Twister (투포원 연사기용 스핀들 유니트의 동특성 해석에 관한 연구)

  • Kim, Gwang-Yeong;Kim, Jong-Su
    • 연구논문집
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    • s.27
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    • pp.127-139
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    • 1997
  • Two-for-one twister is a kind of textile machine and makes special fancy yarn which is twisted two times per one revolution in order to increase tensile strength and wear resis-tance of yarn. Spindle mechanism has to be stable and continuous motion in high speed revolution, and then optimal design is necessary to analyze dynamic characteristics of spindle unit. Spindle unit is consist of blade and rotary disc that are cylindrical body of revolution. For analysis of the dynamic characteristics of spindle unit, transfer matrix method is used and a numerical code SPINDLE also. Torsion and natural bending frequency of the spindle unit are examined. Its displacement mode is studied in function of variable revolutions.

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Spin-Stabilization for the Second Stage of Korea Sounding Rocket-III (KSR-III 탑재부 스핀안정화 기법 연구)

  • Sun, Byung-Chan;Choi, Hyung-Don
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.7
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    • pp.137-143
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    • 2002
  • This paper concerns the spin-stabilization for the second stage of KSR-III(Korea Sounding Rocket-III). The error sources in the second stage are defined, and then the effect on attitude error of KSR-III is analyzed quantitatively and qualitatively. Based on the analysis, some conditions for optimal spinning frequency and optimal steady-spinning duration are suggested. Among several solutions, an optimal value can be determined in the point of minimum impact-point error. An approach to a sub-optimal solution is also suggested. Application to the KSR-III shows that a proper spinning frequency and a steady-spin duration to give the smallest impact-point error can be effectively determined.

How Factors Inside University Can Influence Technology-Based Spin-offs? (대학 내부 특성이 기술기반 스핀오프에 미치는 영향 연구)

  • Kim, HanJun;Kim, YoungJun
    • Journal of Korea Technology Innovation Society
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    • v.21 no.2
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    • pp.560-586
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    • 2018
  • This study empirically analyzes how factors inside university influence the creation of technology-based spin-offs, employing unique data sets. We posit a two-year time lag between the explanatory variables and the dependent one using total 270 university data sets for 5 years in Korea. The results show that universities with experienced technology licensing offices (TLO), those with R&D personnel size, those in possession of incubation policies or business incubators have an edge in creating technology-based spin-offs. The findings provide policy implications. By making more informed decisions on fostering technology-based spin-offs at universities, policymakers can promote the creation of new industries and lead them to create jobs in line with the national economic growth policy.

How Do Research Capabilities and Financial Resources Affect Professors' Entrepreneurship?: Using the Speed of University Spin-off Formations (교수의 연구역량과 연구비 수혜가 대학스핀오프 기업 형성 속도에 미치는 영향)

  • Cho, Sul-Ah;Kang, Ki-H.;Kang, Jin-A
    • Journal of Technology Innovation
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    • v.19 no.2
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    • pp.99-128
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    • 2011
  • University-to-industry technology transfer has become an increasingly important issue in recent years. Studies on technology transfer and commercialization evolved to diverse knowledge transfer channels. Among them, university spin-off is not only known as the most direct and tangible method but also suitable for effectively transferring tacit knowledge. Much of the studies on university spin-offs are mostly focused on macro-level but studies using the individual professors as their unit of analysis need better understanding as well. This paper investigates why the speed of university spin-off formations differ among individual professors drawing on the resource-based view. Utilizing data of 149 professors in 25 universities who formed spin-offs, Cox regression results suggest that professors' technological research capabilities, academic research capabilities and financial resources promote university spin-off formations.

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