• 제목/요약/키워드: Hydrazine

검색결과 399건 처리시간 0.044초

단일 하이드라진 추력기 개발에 관한 고찰 (Review on Mono-hydrazine Thruster Development)

  • 이성택;이상희;최영종;류정호
    • 한국추진공학회지
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    • 제3권1호
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    • pp.72-77
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    • 1999
  • 60년대 이후 위성체 보조추진체계에 가장 널리 채택되고 있는 단일 하이드라진 추력기는 국내에서 다목적실용위성 자세제어용으로 국산화 제작되었다. 본 고찰에서는 이러한 단일 하이드라진 추력기의 설계/제지/시험에 대한 개괄적인 기술적 사항을 수록하고 향후 위성체 및 발사체, 유도미사일에 소요되는 여러 형태의 소형 추력기 국산화 개발을 위해 선행되어야 할 핵심기술분야를 제시해 보았다.

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1-Isonicotinoyl-2-furfurylidene Hydrazine-Cu(II) 착화합물에 관한 분석화학적연구 (Studies on 1-Isonicotinoyl-2-furfurylidene hydrazine-Cu(II) Complex Compound.)

  • 백남호;최윤수
    • 약학회지
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    • 제9권1_2호
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    • pp.18-22
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    • 1965
  • A new organic reagent, 1-isonicotinoyl-2-furfurylidene hydrazine was synthesized from isonicotinic acid hydrazide and furfural, gives precipitate with copper(II), mercury(II) and argent(I), whereas, it gives a water soluble yellow complex with iron(III). Copper complex of the reagent is soluble in EtOH MtOH, pyridine, dioxane and dimethylformamide with green yellow coloration. The complex has a maximum absorption at 385 m.$\mu$ and molar ratio of copper; reagent was estimated as 1:1 by continuous variation method, slop method and chelate titration method. Molar extinction coefficient (9600) and apparant formation constant of this complex was spectrophotometrically determined. K=1.7 * $10^{7}$ (Babko's method) K=2.1 * $10^{7}$ (Anderson's method). This reagent reacted with copper so sensitive that it would be available for determination of Cu (II).

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Arcjet Thruster 유동의 전산해석 (NUMERICAL FLOW FIELD ANALYSIS OF AN ARCJET THRUSTER)

  • 신재렬;최정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.101-105
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    • 2006
  • The computational fluid dynamic analysis has been conducted for the thermo-chemical flow field in an arcjet thruster with mono-propellant Hydrazine (N2H4) as a working fluid. The Reynolds Averaged Navier-Stokes (RANS) equations are modified to analyze compressible flows with the thermal radiation and electric field. The Maxwell equation, which is loosely coupled with the fluid dynamic equations through the Ohm heating and Lorentz forces, is adopted to analyze the electric field induced by the electric arc. The chemical reactions of Hydrazine were assumed to be infinitely fast due to the high temperature field inside the arcjet thruster. The chemical and the thermal radiation models for the nitrogen-hydrogen mixture and optically thick media respectively, were incorporated with the fluid dynamic equations. The results show that performance indices of the arcjet thruster with 1kW arc heating are improved by amount of 180% in thrust and 200% in specific impulse more than frozen flow. In addition to thermo-physical process inside the arcjet thruster is understood from the flow field results.

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히드라진과 질산니켈-아연과의 반응에서 얻은 활성화시킨 촉매를 이용한 방향족 니트로화합물의 환원 (Reduction of Nitroarenes with Hydrazine Monohydrate by Activated Nickel Nitrate-Zinc Catalyst)

  • 윤태호;표상현;박문규;한병희
    • 대한화학회지
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    • 제38권5호
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    • pp.397-403
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    • 1994
  • 질산니켈과 아연을 에탄올 용매하에서 환류반응시켜 얻은 활성화시킨 촉매는 히드라진 존재하에서 방향족 니트로화합물을 주로 아족시 화합물로 환원시켜 주었다. 그러나 질산니켈 대신 염화니켈을 사용하여 얻은 촉매는 같은 조건하에서 단지 방향족 아민만을 얻을 수 있었다. 활성화시키지 않고, 방향족 니트로화합물, 염화니켈이나 질산니켈, 아연 그리고 히드라진 혼합물을 환류반응 시킬 때는 낮은 수율의 아조, 아족시와 아민 화합물을 얻을 수 있었다.

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Preparation of Silver Nanocolloids Using Silver Alkylcarbamate Complex in Organic Medium with PVP Stabilizer

  • Park, Hyung-Seok;Park, Heon-Su;Gong, Myoung-Seon
    • Bulletin of the Korean Chemical Society
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    • 제31권9호
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    • pp.2575-2580
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    • 2010
  • We present a method for chemically reducing silver alkylcarbamate complex with hydrazine to synthesize silver nanocolloids in an organic solvent using polyvinylpyrrolidone (PVP) as the stabilizer. To determine the optimal conditions for preparing stable silver colloids of controlled size and shape, the silver 2-ethylhexylcarbamate (Ag-EHCB) complex, PVP, hydrazine, and 2-propanol solvent concentrations in the reaction mixture were varied. The initial colloid has a mean particle diameter of 5-80 nm, and it exhibits an absorption band with various shapes in the UV region with a maximum near 420 nm. UV-vis spectroscopy, TEM, and X-ray diffraction techniques were used to investigate the formation and growth process of the metallic silver nanocolloids.

Trichloroethylideneacetophenone과 hydrazine들의 반응 (I) pyrazoline 및 pyridazinone 유도체의 합성 (Reactions of trichloroethylideneacetophenone with hydrazines (I) synthesis of pyrazoline and pyridazinone derivatives)

  • 이윤영;이우영;장세희
    • 대한화학회지
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    • 제14권1호
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    • pp.61-64
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    • 1970
  • trichloroethylideneacetophenone과 hydrazine hydrate의 반응으로 3-phenyl-5-trichloromethyl-2-pyrazoline을 합성하였다. 또한 trichloroethylideneacetophenone과 phenylhydrazine 또는 치환된 phenylhydrazine의 반응으로 pyridazinone 유도체들을 합성하였다.

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Surface Properties of the Hydrazinolyzed Poly(ethylene terephthalate)/Nylon 6 Fibers

  • Park, Hyeong-Sup;Gi, Moon-Seong;Jeong, Seok-Kyu;Park, Soo-Min
    • 한국섬유공학회:학술대회논문집
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    • 한국섬유공학회 1996년도 춘계학술발표회 논문집
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    • pp.158-161
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    • 1996
  • Microfibers of Poly(ethylene terephthalate)(PET)/Nylon 6 (P/N) was heat set at 170C in a fixed state and then treated with hydrazine at 30C for 5, 10, 15, 20, 30 and 40 h. Weight loss from the hydrazine treatment increased according to the hydrazine concentration(Fig.1). In order to investigate in detail the effect of the electrostatic attraction between the dye anion and hydrazide groups in cooperated by hydrazinolysis, -potential of P/N fiber was measured by streaming potential method. The surface charge density, o, of the fiber was evaluated from the -potential.

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Hydrazine/Methanol 처리에 의한 PET Film의 미세구조의 변화 (Fine Structural Change of PET Film Treated with Hydrazine Hydrate in Methanol)

  • Sung, Woo-Kyung;Cho, Hyun-Hok;Kim, Kyung-Hwan
    • 한국염색가공학회지
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    • 제2권2호
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    • pp.1-6
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    • 1990
  • In order to investigate the fine structural changes of poly (ethylene terephthalate) film by hydrazinolysis, PET was treated with hydrazine hydrate in methanol at $30^{\circ}C$ for various times. Initially apparent crystallite size and degree of orientation are increased and then, gradually decreased with hydrazinolysis. According to thermoluminescence measurement, trap site decreased by dissolution and then gradually increased with growth of defect in structure. Maximum peak temperature of tan and dynamic loss modulus E" upon hydrazinolysis shifted to the lower temperature in the progress of hydrazinolysis.ysis.

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Kinetic and Molecular Orbital Stuides on the Reaction of 5-nitrofurfural Hydrazone Formation

  • Lee, Kyung-Hee;Jee, Jong-Gi
    • Bulletin of the Korean Chemical Society
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    • 제6권5호
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    • pp.280-284
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    • 1985
  • Kinetic measurements of the 5-nitrofurfural-hydrazine reaction in various pH ranges of aquous solution were carried out by ultraviolet spectrophotometry at $25^{\circ},\;35^{\circ}\;and\;45^{\circ}C$. The observed rate of the reaction varies with the change in pH, which gives characteristic "bell-type" rate acidity profile. The maximum rate is shown in the vicinity of pH 4. This reaction procceds with rate-determining attack of hydrazine on the 5-nitrofurfural at low pH and undergoes a change in rate-determining step to dehydration of the addition intermediate as pH increases. The reaction has a "reactant-like transition state" which precedes intermediate in low pH and "product-like transition state" which follows it in neutral pH. The geometry of 5-nitrofurfural-hydrazine intermediate was estimated with PCILO method associated with CNDO/2 scheme.

Development Status of Iridium Catalyst for Hydrazine Decomposition

  • Kim, S.K.;Lee, K.H.;Yu, M.J.;Cho, S.J.;Lee, J.W.
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.272-274
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    • 2008
  • A development of hydrazine decomposition catalyst for monopropellant thruster has been performed by Korea Aerospace Research Institute(KARI). The goal of this development is to product a catalyst showing the equivalent performance with space-proven catalysts. Catalyst production and physical/chemical analysis were conducted by Chonnam National University and the analysis result was compared with the result of other catalysts and our own specification. Using the developed prototype catalyst, short firing test was performed in a reactor to verify basic performance of catalyst. After the successful reactor test, hot firing tests were carried out in atmospheric and vacuum condition using 5N thruster to verify durability and safety of catalyst. In this paper, the catalyst development status will be presented.

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