• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.137-139
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• 2004

The monopropellant hydrazine thrusters are widely used for the satellite on-board propulsion system fulfilling various missions in space. They have outstanding features caused by the nearly unlimited restart capability and the very high credibility. The sole monopropellant thruster used at precent in nation is MRE-1 that is a standard component of NASA. It can produce 4.45 N of nominal thrust. Due to the glowing complexity with a satellite mission, the needs for thrusters of the diverse performance are being increased. The numerical simulation could give useful information to develop a new type thruster instead of the experiments performed previously. Therefore it is critical to make a reliable computer code to prepare design change of a thruster. In this paper, the performance analysis and validation of the satellite monopropellant hydrazine thruster currently used is accomplished as the preliminary study to serve valuable data for future design change.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.151-154
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• 2007

본 연구는 추력기 기초 설계개념 확보를 위한 주요 요소기술로서 촉매대 설계인자 및 하이드라진 분해촉매의 분해거동을 파악하는 것을 목적으로 한다. 이를 위해 저궤도 위성용으로 적용되고 있는 1Lbf급 하이드라진 추력기의 설계 제원을 기초로 하여 가시화 반응기를 설계/제작하였으며, 촉매대의 분해반응 및 거시적 거동을 육안 관찰함으로서 촉매대 설계개념을 파악하고자 하였다.

• 대한화학회지
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• 제15권4호
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• pp.183-189
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• 1971

Stoichiometry of hydrazine-bromate reaction has been studied in acid media of varying compositions, elucidating the effects of bromide and chloride ions in sulfuric acid, perchloric acid, hydrochloric acid, and hydrobromic acid at varying concentrations of hydrogen ion and cupric ion. The study shows that the number of red-ox equivalent consumed by one mole of hydrazine becomes practically 4.00 if the concentrations of bromide and hydrogen ions are kept higher than 0.1M and 6M, respectively. The presence of copper tends to reduce the bromate consumption by hydrazine in an irregular manner, but such an effect becomes unimportant if the concentrations of bromide and hydrogen ions are kept sufficiently high.

• 한국분말재료학회지
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• 제22권4호
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• pp.260-265
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• 2015

Spherical fine cobalt powders were fabricated by new liquid reduction method. Commercial cobalt sufate heptahydrate was used as raw material. Also ethylene glycol was used as solvent and hydrazine-sodium hypophosphite mixture was used as reduction agent for the new liquid reduction method. A plate shaped cobalt powders with an approximately 300 nm were prepared by a traditional wet ruduction method using distilled water as solvent and hydrazine. Spherical fine cobalt powders with an average size of $1-3{\mu}m$ were synthesized by a new liquid reduction method in 0.3M cobalt sulfate and 1.5M hydrazine-0.6M sodium hypophosphite mixture at 333K.

• Journal of Electrochemical Science and Technology
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• 제5권3호
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• pp.73-81
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• 2014

This paper describes the continuous flow operation of membraneless sodium perborate fuel cell using acid/alkaline bipolar electrolyte. Here, hydrazine is used as a fuel and sodium perborate is used as an oxidant under Alkaline-acid media configuration. Sodium perborate affords hydrogen peroxide in aqueous medium. In our operation, the laminar flow based microfluidic membranleless fuel cell achieved a maximum power density of $27.2mW\;cm^{-2}$ when using alkaline hydrazine as the anolyte and acidic perborate as the catholyte at room temperature with a fuel mixture flow rate of $0.3mL\;min^{-1}$. The simple planar structured membraneless sodium perborate fuel cell enables high design flexibility and easy integration of the microscale fuel cell into actual microfluidic systems and portable power applications.

• 한국산학기술학회:학술대회논문집
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• 한국산학기술학회 2004년도 추계학술대회
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• pp.255-258
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• 2004

Hydrazine is a weak base and strong reducing agent in the aqueous solution and is primarily utilized as a high-energy rocket propellant and an oxygen scavenger in boiler or feedwater. The objective of this study was to investigate the physicochemical properties and reactions of hydrazine and the catalytic and thermal decomposition by the temperature change. Hydrazine was fast decomposed with the catalyst of lower activation energy and at the higher temperature.

• Bulletin of the Korean Chemical Society
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• 제35권8호
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• pp.2448-2452
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• 2014

Second-order rate constants ($k_N$) have been measured spectrophotometrically for $S_NAr$ reactions of Y-substituted-phenoxy-2,4-dinitrobenzenes (1a-1g) with hydrazine and glycylglycine in 80 mol % $H_2O$/20 mol % DMSO at $25.0{\pm}0.1^{\circ}C$. Hydrazine is 14.6-23.4 times more reactive than glycylglycine. The magnitude of the ${\alpha}$-effect increases linearly as the substituent Y becomes a stronger electron-withdrawing group (EWG). The Br${\o}$nsted-type plots for the reactions with hydrazine and glycylglycine are linear with ${\beta}_{lg}=-0.21$ and -0.14, respectively, which is typical for reactions reported previously to proceed through a stepwise mechanism with expulsion of the leaving group occurring after rate-determining step (RDS). The Hammett plots correlated with ${\sigma}^{\circ}$ constants result in much better linear correlations than ${\sigma}^-$ constants, indicating that expulsion of the leaving group is not advanced in the transition state (TS). The reaction of 1a-1g with hydrazine has been proposed to proceed through a five-membered cyclic intermediate ($T_{III}$), which is structurally not possible for the reaction with glycylglycine. Stabilization of the intermediate $T_{III}$ through intramolecular H-bonding interaction has been suggested as an origin of the ${\alpha}$-effect exhibited by hydrazine.

• 공업화학
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• 제30권6호
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• pp.652-658
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• 2019

하이드라진 직접 액체 연료전지는 이산화탄소를 배출하지 않으며, 높은 에너지 밀도를 가지고, 귀금속 촉매를 사용하지 않고도 높은 촉매 활성을 보이는 장점으로 유망한 연료전지로써 활발히 연구가 진행되어 왔다. 하지만, 고안전성 연료전지 운전 성능을 위해서는 전극촉매를 비롯한 핵심소재 개발 및 성능 연구를 토대로 연료의 물질전달 특성을 비롯한 하이드라진 연료전지 내에서 진행되고 있는 작동 프로세스를 충분히 이해할 필요성이 있다. 본 논문에서는 최근의 직접 하이드라진 연료전지 연구결과 중에 가격 경쟁력을 확보한 전극촉매 및 연료 확산, 물 관리, 기체 발생 측면에서 전극 구조 개발 동향을 소개하며 향후 개발 방향에 대해서 고찰하고자 한다.

• 대한화학회지
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• 제46권5호
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• pp.462-483
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• 2002

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.139-142
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• 2011

본 연구팀에서 개발 중인 하이드라진 추력기의 설계성능 검증에 앞서 요소부품인 비충돌형 인젝터에 대한 인수시험 및 수류시험을 수행하였다. 실험에 사용된 인젝터는 추진제 주입압력 24.6 $kg_f/cm^2$에서 70 N의 공칭추력을 내는 하이드라진 추력기에 장착되는 것이다. 각각의 인젝터 노즐 오리피스의 미세한 가공오차에 기인하여 미립화 특성 차이가 관찰되기는 하였으나, 인젝터 분사각 관련 성능평가에서는 모든 오리피스가 합격범위에 있음이 확인되었다.