• Journal of the Society of Disaster Information
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• v.12 no.3
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• pp.286-291
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• 2016

In this study, we conducted about the manufacture of a non-combustible inorganic insulation by replacing the binder type for satisfaction of thermal conductivity for developing a lightweight inorganic insulation. Thermal conductivity was measured using a machine of HFM-436. We made samples are inorganic insulation by using SH-1(liquid) of S company and SH-2(solids). By Mixing Pearlite and SH-4(Liquid) was produced as insulation sample 2. Each was shaped into a binder and pearlite in the frame. After complete drying, thermal conductivity was measured by using HFM-435. The thermal conductivity was determined using two different binder. We analyzed the effect on thermal conductivity in binder.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1997.11a
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• pp.5-5
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• 1997

고체추진제에 대한 비선형 점탄성 구성모델이 제시되었다 추진제 손상의 원인으로서 바인더와 AP 충전제사이의 접착분리를 고려하였으며, 점탄성 드웨팅판별식이 개발되었다. 손상에 의한 추진제의 연화는 모듈러스 저하로서 취급되었으며, 모듈러스저하 계산시에 드웨팅에 의하여 야기된 미소진공구의 모듈러스는 유한 상수로서 간주되었다. 바인더와 AP 충전제사이의 접착에너지는 180$^{\circ}$ 접착박리시험으로 측정하였다. 반복하중시의 비선형성은 전단변형률 불변량의 함수로서 고려되었다. 이 구성모델은 여러 하중조건에 대한 시편실험과 비교되어 잘 일치하였으며, 복잡한 미시구조학적 역학기구 없이 간단하게 고체 추진제의 거동을 예측할 수 있게 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.28-28
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• 2000

HTPB/AP/AI 추진제는 none-reinforcing filler가 다량 함유되어 있어 기계적 특성은 바인더와 고체 충진제의 계면 접착력에 따라 크게 영향을 받으며 이를 향상시키기 위해 결합제의 연구가 다수 진행되었고 추진제의 인장 변형율을 증가시키기 위해 HTPB의 관능기수에 따른 가교밀도, 경화제와 경화촉매, 가소제등 최적의 바인더조성을 위해 가능한 원료 및 함량 연구에 많은 노력을 기울여 왔다. 또한 추진제의 주원료로서 AP는 추진제의 성능 및 내탄도 관점에서 입자크기에 따른 연소특성 및 고성능을 위한 충전 분율에 대해 주로 연구되었으며 특히 Oberth와 Farris는 고체추진제 분야에서 많은 업적을 이루었다.(중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.181-184
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• 2009

A development of a composite solid propellant is carried out for an application to gas generators as an energy source of rocket system. With HTPB as a propellant binder which has 80% of particle loading ratio, a favorable rheology, and moderate curing properties at the range of $-50^{\circ}C{\sim}70^{\circ}C$, AN is selected as the first kind of oxidizer having the characteristics of a low flame temperature, minimal particle residual as well as nontoxic products. AP is the second oxidant for ballistic property control. A series of experiments for the improvement of physical properties were conducted and resulted in the propellant formulation having 30% of strain rate at 8 bar of max. stress.

• Journal of the Korean Electrochemical Society
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• v.19 no.3
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• pp.107-113
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• 2016

In this study, an anion-exchange ionomer solution was prepared by grinding poly(2,6-dimethyl-1,4-phenylene oxide) (PPO) in liquid nitrogen for solid alkaline fuel cells (SAFCs). Type of quaternized PPO (QPPO) solutions was controlled by grinding time. The ionomer binder solutions were characterized in terms of dispersity, particle size, and electrochemical properties. As a result, ionomer binder solutions using grinded polymer showed higher dispersion and smaller particle size distribution than that using non-grinded polymer. The highest ionic conductivity and IEC of the membrane recast by using BPPO-G120s were $0.025S\;cm^{-1}$ and $1.26meq\;g^{-1}$, respectively.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.4
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• pp.31-37
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• 1999

Recently, the development of propellant trends toward minimum smoke signature, insensitivity and high performance. PSAN has been used as a oxidizer for less sensitive minimum smoke propellant. Unfortunately, it provides low performance to propellant. Energetic polymers such as GAP and PGN are frequently proposed for use in minimum smoke Propellants to overcome the energy Penalty imposed by using AN as the oxidizer. In this study the mechanical properties, glass transition temperature and viscosity of PGN and EPGN binder were investigated.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.5
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• pp.1-6
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• 2009

A development of a composite solid propellant is carried out for an application to gas generators as an energy source of rocket system. With HTPB as a propellant binder which has 80% of particle loading ratio, a favorable rheology, and moderate curing properties at the range of $-50^{\circ}{\sim}70^{\circ}C$, AN is selected as the first kind of oxidizer having the characteristics of a low flame temperature, minimal particle residual as well as nontoxic products. AP is the second oxidant for ballistic property control. A series of experiments for the improvement of physical properties were conducted and resulted in the propellant formulation having 30% of strain rate at 8 bar of max. stress.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.495-497
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• 2017

Thermoplastic propellants using thermoplastic elastomer binders show moderate performance and mechanical properties compared to thermoset propellants, but these propellants are widely used in a variety of fields due to low cost of raw materials, simple manufacturing process and stable handling process. In order to utilize thermoplastic solid propellants in various fields, we will study properties depending on the content of oxidants, metal fuels and additives.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.1
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• pp.95-103
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• 1999

Low pressure combustion characteristics of the composite solid propellants were studied in terms of the propellant burning rate, ignition processes, and the structure of the extinguished surfaces. Optical Vacuum Strand Burner(OVSB) system was designed and configured for this purpose. Burning rates of the propellants were measured at subatmospheric pressure by developed test method in OVSB. The ignition and combustion phenomena of the studied propellants in the combustion chamber of OVSB were recorded and analyzed with the camera and VCR(30 frames/s). Burning surfaces of the propellants were extinguished by rapid depressurization method and analyzed with Scanning Electron Microscope(SEM).

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.21-21
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• 1998

Polyethylene glycol(PEG) 또는 polycaprolactone(PCP)을 예비 중합체로 사용하고 butanetriol trinitrate와 diethylene glycoldinitrate를 가소제로, cyclo-tetramethylene tetranitramine을 주산화제로 사용한 고체 추진제를 제조하여 이들의 기계적 성질을 증진시키기 위한 연구를 하였다. PEG의 일부를 PCP로 대체 시 추진제의 기계적 성질은 증가하며 PCP만 사용시 추진제의 최대 인장 강도는 PEG만 사용시 보다 약 17%, 최대 응력 하에서의 신율은 약 59% 그리고 탄성 계수는 약 9% 증가한다. 그러나 예비 중합체로 PCP만을 사용한 추진제는 4$0^{\circ}C$, 90% 상대 습도하에서 보관시 추진제의 경도 변화 실험에서 6주 후에 경도가 0이 되며, 위의 조건하에서 보관 기간에 따른 PCP 바인더의 부피 팽윤 실험에 의해 초기 부피 팽윤 비와 팽윤비의 변화 속도가 PEG를 혼용한 바인더보다 크므로 PCP 사용시 수분에 대한 안정성은 저하됨을 알 수 있었다.