• Title/Summary/Keyword: Defense R&D

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Analysis of Boundary Layer in Solid Rocket Nozzle and Numerical Analysis of Thermal Response of Carbon/Phenolic using Finite Difference Method (고체 로켓 노즐의 경계층 해석과 유한차분법을 이용한 탄소/페놀릭의 열반응 해석 연구)

  • Seo, Sang Kyu;Hahm, Hee Cheol;Kang, Yoon Goo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.1
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    • pp.36-44
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    • 2018
  • The thermal response of carbon/phenolic used in a solid rocket nozzle liner was analyzed. In this paper, the numerical analysis of the thermal response of carbon/phenolic consists of (1) the integration equation of the boundary layer to obtain the convective heat transfer coefficient of the combustion gas on the rocket nozzle wall and (2) 1-D finite difference method for heat conduction of carbon/phenolic to calculate the ablation, char, and temperature. The calculated result was compared with the result of a blast-tube-type test motor. It is found that the calculated result shows good agreement with the thermal response of the test motor, except at the vicinity of the throat insert.

Study on the Priority of Defense R&D Project for Verifying Weapon Systems Requirement (전력소요 통합검증을 위한 국방 R&D사업 우선순위 선정에 관한 연구)

  • Lee, Ho-Jin;Ahn, Nam-Su
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.5
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    • pp.153-159
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    • 2018
  • In recent years, the development of weapons systems in the field of defense research and development has become increasingly large, complex, and long-term, and so have budgets and the time spans involved. In order to improve this, the Weapon Systems Requirement Verification Committee, which benchmarked the preliminary feasibility of the private sector, was established to verify the appropriateness of requirements, and the necessity and priority of the projects. This research proposes a methodology for analyzing and prioritizing proposed weapons systems for effective and strategic allocation of defense budget funding. First, the evaluation factors that can be used in the defense sector were assessed by analyzing the related fields. We set the weighting of items by using the analytical hierarchy process for technical risk assessment and technical profitability evaluation. After that, we applied the methodology to 32 weapons systems and analyzed the results. In conclusion, through this study, it was possible to analyze profitability dimensions overlooked in the existing methodology.

SAR Test-bed to Acquire Raw Data and Form Real-time Image (실시간 영상형성 및 원시데이터 획득용 SAR 테스트 베드)

  • Shin, Hyun-Ik;Kwon, Kyoung-Il;Yoon, Sang-Ho;Kim, Hyung-Suk;Hwang, Jeonghun;Ko, Young-Chang;You, Eung-Noh;Kim, Jin-Woo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.20 no.2
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    • pp.181-186
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    • 2017
  • Synthetic aperture radar(SAR) has been widely used for reconnaissance. It provides high-resolution, day-and-night and weather-independent images for a multitude of applications. Because SAR coherently combines many viewing angles to effectively create a large aperture(narrow beam) radar, the test-bed should be capable of moving straightly SAR sensor for the integration angle to meet resolution. This paper describes the test-bed developed to test and evaluate the SAR performance. It forms high-quality images in real time and saves the raw data for the purpose of post processing on the ground.

Development and Verification of Lightning Induced Transient Protection Device for Avionics Computer (항공기 탑재 컴퓨터용 간접낙뢰 보호장치 개발 및 검증)

  • Sim, Yong-gi;Ahn, Tae-sik;Park, Jun-hyun;Han, Jong-pyo;Yang, Seo-hee
    • Journal of Advanced Navigation Technology
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    • v.19 no.5
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    • pp.395-402
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    • 2015
  • This paper introduces the design details and test procedures of the lightning induced transient protection device for protecting the damage caused by indirect lightning strike on the computer mounted on the aircraft. Lightning induced surge voltage is bring a malfunction or damage to the aircraft electrical and electronic equipment, that is referred to indirect effects of lightning. In order to protect the electronic equipment on aircraft from the indirect effects of lightning, that is achieved by analyzing the effect on aircraft from lightning and protect design for each devices. In this paper, we introduce an indirect lightning strike level decisions, the protection circuit design method according to the chosen level through the RTCA DO-160G Section 22 category analysis and selection was performed in order to protect the damage caused by indirect lightning strikes in the protected equipment. In addition, we show the indirect lightning effects verification test performed to validate the designed protection circuits.

Characteristics of Stimulated Brillouin Scattering Suppression in High-power Fiber Lasers Using Temperature Gradients (온도구배에 의한 고출력 광섬유 레이저의 유도 브릴루앙 산란 억제 특성)

  • Jeong, Seongmook;Kim, Kihyuck;Lee, Sunghun;Hwang, Soonhwi;Yang, Hwanseok;Moon, Byunghyuck;Jhon, Young Min;Park, Min Kyu;Lee, Jung Hwan
    • Korean Journal of Optics and Photonics
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    • v.30 no.4
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    • pp.167-173
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    • 2019
  • In this paper, we studied characteristics of stimulated Brillouin scattering (SBS) suppression in high-power fiber lasers by using apparatuses applying a temperature gradient (i.e. a step, a sine shape, and random temperature distribution) along the fiber. From the ytterbium-doped polarization-maintaining fiber master oscillator power amplifier built in house, we measured the back-reflection spectrum and power for each temperature gradient, showing that the step shape temperature distribution was the most effective way to suppress SBS. In addition, we investigated the interaction of pseudo-random binary sequence phase modulation conditions and temperature gradients for SBS suppression.

Pyroshock Measurement and Characteristic Analysis of Explosive Bolt and Pyrotechnic Initiator (폭발볼트와 착화기의 파이로충격 계측 및 특성 분석)

  • Lee, Juho;Hwang, Dae-Hyun;Jang, Jae-Kyeong;Lee, YeungJo;Kim, Dong-Jin;Lee, Jung-Ryul;Han, Jae-Hung
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.27 no.2
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    • pp.213-220
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    • 2017
  • Pyroshock produced by the pyrotechnic devices can induce failures in nearby electronic devices. To handle and mitigate pyroshock inducing problems, appropriate measurement of pyroshock is essential. In this study, pyroshock measurement technique is established using laser Dopper vibrometers (LDVs) and shock accelerometers. Pyroshock produced by the explosive bolts and the pyrotechnic initiators under various environments is measured. The characteristics of pyroshock including the effects of supporting structures, propagation form on thin plate, sensor (contact and non-contact) types are discussed.

Estimation of Jamming Parameters based on Gaussian Kernel Function Networks (가우스 요소함수 망에 기초한 재밍 파라미터 추정)

  • Hwang, TaeHyun;Kil, Rhee Man;Lee, Hyun Ku;Kim, Jung Ho;Ko, Jae Heon;Jo, Jeil;Lee, Junghoon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.23 no.1
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    • pp.1-10
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    • 2020
  • Effective jamming in electronic warfare depends on proper jamming technique selection and jamming parameter estimation. For this purpose, this paper proposes a new method of estimating jamming parameters using Gaussian kernel function networks. In the proposed approach, a new method of determining the optimal structure and parameters of Gaussian kernel function networks is proposed. As a result, the proposed approach estimates the jamming parameters in a reliable manner and outperforms other methods such as the DNN(Deep Neural Network) and SVM(Support Vector Machine) estimation models.

The Characteristic Analysis and the Manufacture of Explosive THPP on PMD (PMD용 화약 THPP 제조 및 특성분석)

  • Kim, Sangbaek;Shim, Jungseob;Ahn, Gilhwan;Kim, Junhyung;Ryu, Byungtae
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.5
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    • pp.84-89
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    • 2016
  • THPP(Titanium Hydride Potassium Perchlorate) is an igniter composed of potassium perchlorate as oxidizing agent and titanium hydride as fuel with a Viton binder. THPP is commonly found in the aerospace, defence and automotive industries. This research is investigeted for the manufacturing process and characteristics analysis of the THPP such as the performance and shape/calorimetry/pressure characteristics of the THPP on PMD(Pyrotechnic Mechanical Device). Also, THPP composite ratio is designed by CEA program.

Design of a Single Pulse Laser Range Finder with Er:Yb:glass Microchip Lasers (어븀:이터븀:유리 마이크로칩 레이저를 이용한 단펄스 거리측정기 설계)

  • Koh, Hae Seog;Lee, Chang Jae;Park, Choong Bum;Jeon, Hyoung Ha;Ahn, Pil Dong;Park, Do Hyun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.21 no.3
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    • pp.295-305
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    • 2018
  • We present a passively Q-switched monolithic Er:Yb:glass microchip laser developed in our lab. The microchip laser can produce pulses at 1535 nm of the 'eye-safe' wavelengths with the pulse energy of 50 uJ and the pulse width of 4-6 ns. Using the laser we also designed and developed a pulsed Er:Yb:glass microchip laser rangefinder. Expressions for background and signal power, noise, and signal-to-noise ratio are reviewed. A computer simulation was used to optimize laser power, receiver aperture, and preamplifier bandwidth for the efficient system design of the laser rangefinder. Experimental results are presented to compare with the theory.

Characteristic Property of Combustion and Internal Ballistics of Triple-Based Propellant including RDX (RDX를 적용한 다기추진제의 연소 및 강내탄도 특성)

  • Son, Soojung;Lee, Wonmin;Lee, Woojin;Kwon, Soonkil;Jung, Jinyoung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.3
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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.