• 접착 및 계면
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• 제12권3호
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• pp.94-98
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• 2011

열경화성 및 열가소성 우레탄 수지 첨가에 따른 헤라크론/페놀수지 복합재료의 방탄성능 변화를 고찰하였다. 먼저 페놀 또는 우레탄 수지를 헤라크론 직조섬유에 스프레이 코팅하여 프리프레그를 제조하고, 이들의(페놀/우레탄) 비율을 변화시켜 16층의 복합재료를 $150^{\circ}C$에서 $150kg/cm^2$의 압력으로 25 min간 성형하여 제조하였다. 방탄성능은 1.1 g 모의파편탄(22 cal)으로 분석하였으며, 우레탄 수지의 종류 및 페놀/우레탄 프리프레그의 비율에 따른 V50 변화를 고찰하였다.

• Composites Research
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• 제18권6호
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• pp.34-39
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• 2005

본 연구에서는 방탄재료로 활용 가능할 것으로 예상되는 여러 구조용 세라믹스의 물리기계적 물성과 방탄물성과의 상호연관성을 분석하였다. 물리기계적 물성을 측정한 후 30mm 고체추진포에서 10.7의 L/D비를 갖는 텅스텐 긴 관통자를 비행시켜 운동에너지(KE)탄에 대한 방탄물성을 측정하였으며, K215 자탄을 기폭시켜 성형작약(HEAT)탄에 대한 방탄물성을 측정하였다. 영률/밀도비, 경도/밀도비 및 꺽임강도/밀도비가 증가할수록 방탄물성이 대체적으로 증가하는 경향을 보였으며, 특히 HEL(Hugoniot Elastic Limit)/밀도비가 증가함에 따라 KE탄에 대한 방탄물성이 선형적으로 증가하는 현상을 나타내었다.

• Composites Research
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• 제18권6호
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• pp.48-53
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• 2005

본 연구에서는 방탄물성이 매우 우수한 알루미나-실리카계 방탄재료(PL-8)의 방탄물성을 향상시키기 위해 성형압력 및 소결온도를 변화시켰다. 물리/기계적 물성을 측정 한 후 성형작약(HEAT)/운동에너지(KE)탄에 대한 방탄물성을 측정하여 분석하였다. 그 결과 소결온도 $1235^{\circ}C$에서 성형작약탄에 대한 방탄물성이 가장 높았으며 기 개발된 알루미나-실리카계 방탄재료 (PL-8)에 비해 $22\%$ 방탄물성이 향상되었다.

• 한국세라믹학회지
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• 제29권4호
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• pp.312-318
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• 1992

Two kinds of alumina specimens with different grain size (1 and 51 $\mu\textrm{m}$) but same density were prepared by hot-pressing. Fracture strength and fracture toughness of these specimens at low strain rate, sonic velocity, and elastic property were evaluated. Ballistic performance against Cal. 50 AP projectile was characterized by thick-backing method by using A16061-T6 reference block. Mechanical properties measured at low strain rate showed that the specimen with samll grain (SG) were better than specimen with large grain (LG). Fracture strength and fracture toughness of LG specimen were 131 MPa and 3.01 MPa{{{{ SQRT { m} }}, but those of SG specimen were 349 and 4.23, respectively. Sonic velocity and elastic properties of these specimen were similar, but bulk velocity and bulk modulus were different at amount of 4 and 9%. The tendency of ballistic performance was not consistent with the mechnaical properties at low strain rate. The ballistic performance based on quantitative efficiency revealed that the LG specimen (5.13) was ballistically better than the SG specimen (4.00) in spite of their lower mechanical properties.

• Composites Research
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• 제18권6호
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• pp.40-47
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• 2005

본 연구에서는 세라믹 방탄재료개발을 위해 가장 경제적이고 방탄물성이 높은 알루미나를 기본으로 하여 압축-팽창률이 높은 실리카를 첨가하여 방탄물성이 우수한 세라믹 방탄재료를 개발하고자 하였다. 3가지 조성을 선정하였으며 각각 조성에 적합한 소결온도를 설정하였다. 물리/기계적 물성을 측정한 후 K215 자탄을 기폭시켜 성형 작약(HEAT)탄에 대한 방탄물성을 측정하였으며, 30mm 고체추진포에서 10.7의 L/D비를 갖는 팅스텐 긴 관통자를 비행시켜 운동에너지(KE)탄에 대한 방탄물성을 측정하여 분석하였다. 그 결과 $46\%\;Al_2O_3\;-\;51\%\;SiO_2$가 가장 높은 방탄물성을 나타내었으며 알루미나에 비해 매우 우수한 방탄재료로 평가되었다.

• 한국추진공학회지
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• 제4권3호
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• pp.45-54
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• 2000

Ignition transient is a. very rapid process lasting only in the order of 100 milliseconds and therefore it is difficult to measure all relevant ballistic properties. Numerical simulation is thus useful to quantify some of these hard to measure flow and ballistic properties. One-dimensional model was employed to study the effects of aging using simplified aging scenarios for both N-H sustainer and booster motors. Also the effects of newly designed igniter on the ignition of N-H sustainer was simulated. Radiation effects could be significant in terms of energy flux increase to the propellant surface and the energy exchange between the combustion gas itself. One dimension implementation of radiation showed significant effects for rear-mounted igniter. Implementation of radiation effects into 2-D axi-symmetric numerical model was completed and its effects on the N-H sustainer were examined. To have a reliable prediction of computer model on ignition transient, accurate chemical property data on the propellant and igniter gas are required. It was found that such property data on aged N-H motors are not available. Chemical aging model can be used to predict to some degree of accuracy effects of aging on chemical and mechanical properties. Such a model was developed, albeit 2-dimensional, to study migration of moisture through a representative solid rocket motor configuration.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 추계학술발표대회 논문집
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• pp.83-86
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• 2001

This paper presents an investigation of the contribution of fibers in energy absorption during impact and the effect of resin types on properties of the high strength polyethylene (Spectra-900 PE) composite. In high strength polyethylene fiber, main impact energy absorbing mechanism was tensile breakage and deformation of fiber. Two types of resin were examined : Unsaturated polyester (UP) and Epoxy. Tensile and 3-point bending test have been performed to investigate the changes of mechanical properties. In tensile and flexural testes, the Spectra Composite prepregged with UP showed higher properties than Spectra Composite prepregged with epoxy.

• 제어로봇시스템학회논문지
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• 제13권11호
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• pp.1053-1059
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• 2007

This paper presents a target sate estimator(TSE) with low pass filter for improving the gun driving command. The ballistic computer uses target information such as predicted range, velocity, acceleration of a target to generate the gun command. We adopt the finite impulse response(FIR) filter as our TSE to shorten calculation time for the driving command and due to its inherent stability property. We also introduce a post-processing filter to reduce the high frequency components in the output signal of a TSE which may cause instability of gun driving. The first order low pass filter has been designed based on $H{\infty}$ criteria considering the noise characteristics. To show the validity of the present scheme, simulation results are given for the overall gun driving system including aircraft target information.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.181-184
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• 2009

로켓시스템의 에너지원으로 적용할 수 있는 기체발생기용 복합 고체추진제의 개발과정을 기술한다. 80%의 고체입자 부하율과 양호한 유동성, 그리고 $-50^{\circ}C{\sim}70^{\circ}C$에서 경화에 적절한 추진제 물성을 갖는 HTPB를 바인더로 하여, 낮은 화염온도, 적은 고체입자 잔사, 무독성 생성물의 추진제 제조가 가능한 AN을 제1종 산화제로, 탄도특성 제어에 필요한 AP를 제2종 산화제로 추진제 주요 조성이 구성된다. 기본조성을 근거로 하여 일련의 물성개선 시험이 수행되었으며 최대응력 8 bar 및 최대응력점 변형율 30%, 그리고 탄성계수 1000 psi 수준의 물성을 갖는 추진제 조성을 얻을 수 있었다.

• 한국군사과학기술학회지
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• 제25권3호
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• pp.321-328
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• 2022

The current development tend of the gun propellants that they should have low sensitivity and high energy. We studied a nitrocellulose based propellant composition that replaced sensitive NG with RDX and DEGDN which high energy and low sensitivity. The important factors in the design of the gun propellant were impetus and flame temperature. NC-based propellant containing RDX showed similar impetus but low flame temperature compared to KM30A1, a triple-based propellant. The developed propellant composition didn't show any abnormal combustion reaction and the characteristics of ballistic resistance were also confirmed.