• 제목/요약/키워드: Defence R&D

검색결과 97건 처리시간 0.03초

Synthesis and Characterization of Tetrazine Derivatives as High Energy Propellants (테트라진 계열의 추진 물질 합성 연구)

  • Lee, Woonghee;Park, Youngchul;Joo, Young-Hyuk
    • Journal of the Korean Society of Propulsion Engineers
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    • 제17권6호
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    • pp.38-47
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    • 2013
  • Traditional propellants release toxic gases during combustion that are harmful to the environment. This study describes a novel synthetic process of two high nitrogen containing tetrazines, TATTz and BTATz, which can be adapted as solid fuels for a solution to environmental concerns. The compounds were characterized by NMR, IR spectroscopy, and differential scanning calorimetry(DSC). Detonation properties were calculated with the EXPLO5 program based on calculated heats of formation and measured densities.

Natural Aging Properties Analysis of HTPB Propellant (HTPB계 고체추진제의 자연노화 물성 분석)

  • Park, Jung-Ho;Ryu, Nam-Sun;Park, Jae-Beom;Jung, Gyoo-Dong
    • Journal of the Korean Society of Propulsion Engineers
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    • 제23권1호
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    • pp.9-14
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    • 2019
  • Hydroxy-terminated polybutadiene (HTPB) propellants of solid rocket motors age differently under different storage temperatures. The shelf life of a solid rocket motor depends on the aging ratio of the HTPB propellant; it can be estimated through the viscoelastic properties by an aging test. This study analyzed the initial and natural aging properties during long-term storage. The initial properties were obtained from characterization and accelerated test results. The test results were obtained by analyzing the strain on cylindrical grains when a thermal load was applied.

Proteomic Analysis of Global Changes in Protein Expression During Exposure of Gamma Radiation in Bacillus sp. HKG 112 Isolated from Saline Soil

  • Gupta, Anil Kumar;Pathak, Rajiv;Singh, Bharat;Gautam, Hemlata;Kumar, Ram;Kumar, Raj;Arora, Rajesh;Gautam, Hemant K.
    • Journal of Microbiology and Biotechnology
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    • 제21권6호
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    • pp.574-581
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    • 2011
  • A Gram-positive bacterium was isolated from the saline soils of Jangpura (U.P.), India, and showed high-level of radiation-resistant property and survived upto 12.5 kGy dose of gamma radiation. The 16S rDNA sequence of this strain was examined, identified as Bacillus sp. strain HKG 112, and was submitted to the NCBI GenBank (Accession No. GQ925432). The mechanism of radiation resistance and gene level expression were examined by proteomic analysis of whole-cell extract. Two proteins, 38 kDa and 86.5 kDa excised from SDS-PAGE, which showed more significant changes after radiation exposure, were identified by MALDI-TOF as being flagellin and S-layer protein, respectively. Twenty selected 2-DE protein spots from the crude extracts of Bacillus sp. HKG 112, excised from 2- DE, were identified by liquid chromatography mass spectrometry (LC-MS) out of which 16 spots showed significant changes after radiation exposure and might be responsible for the radiation resistance property. Our results suggest that the different responses of some genes under radiation for the expression of radiation-dependent proteins could contribute to a physiological advantage and would be a significant initial step towards a fullsystem understanding of the radiation stress protection mechanisms of bacteria in different environments.

An Empirical Study on the Effect of R&D Investments on the Business Performance of Defence Industries (방산업체의 연구개발 투자활동이 경영성과에 미치는 실증적 연구)

  • Hwang, Eui-Sang;Song, Young-I1
    • Journal of the military operations research society of Korea
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    • 제34권1호
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    • pp.47-59
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    • 2008
  • This paper deals with an empirical study to statistically analyse various business performance on research and development(R&D) as an independent variables. The major results of statistical analyses have come up with the followings : First, the regression analyses between the growth rate and the opportunity of education showed the positive relationship. Second, the regression analyses between the productivity and the expenses of R&D showed the positive relationship. Third, the regression analyses between the profit and the mutual cooperation showed the positive relationship.

A Study on the Effective Implementation Methodology of Evolutionary Development in Defence Weapon System Research & Development Project (국방 무기체계 연구개발 사업에서 진화적 개발의 실효적 수행 방안에 관한 연구)

  • Kim, Jung Myong;Cha, Seung Hoon;Lee, Hye Jin;Yoo, Jae Sang;Choi, Sang Wook
    • Journal of the Korean Society of Systems Engineering
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    • 제17권1호
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    • pp.35-42
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    • 2021
  • Recent defense R&D projects have been required as weapons systems applied with advanced technology considering exports. As a result, the complexity of the applied technology increases, and the risk of system development increases. Under these circumstances, an effectives method of performing evolutionary development for economical and timely deployment is presented. To this end, we hope that this study, which proposed the maintenance of related laws and measures for realistic and active evolutionary development, will help the R&D of the weapons systems.

Calculation of Sample Size for Guided Missile Considering Test Method and Reliability Growth (유도무기 시험평가 방법과 신뢰성 성장을 고려한 시험 수량 산출)

  • Lee, Youn-ho;Kim, Jae-hwang;Lee, Kye-shin;Lee, Jong-sin;Lee, Myoung-jin;Kim, Doo-hyun
    • Journal of the Korea Institute of Military Science and Technology
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    • 제20권6호
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    • pp.844-852
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    • 2017
  • Since guided weapon is high-cost and one-shot device which is non-reusable, it requires a lot of resources to prove required accuracy as a part of reliability demonstration. Once a test for proving accuracy rate of guided missile fails, it causes an additional cost and delay of schedule. This study introduces an equation for proper sample size and plan for guided-missile accuracy rate test in order to minimize the risk of test failure. Proper sample size for the test is derived by considering the reliability growth. Furthermore, each task for accuracy rate test is defined according to the development step. Therefore, this study can contribute to reduce sample size for accuracy rate test in order to meet the reliability requirement and assure transparency in the test process.

Study on Open Appraisal System Modeling for Government Research and Development Program through Review of Law and Administrative Rules : Focused on Clean Appraisal System (국가연구개발사업에 있어서 제도적 차원의 개방형 평가 시스템 모델링에 관한 연구 : 클린평가시스템을 중심으로)

  • Lee, Dong Han;Jee, Myung Keun;Lee, Ook
    • Journal of Information Technology Services
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    • 제14권4호
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    • pp.45-60
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    • 2015
  • Governments around the world invest in research and development (R&D) for different purposes : national economy, defence, environment, health, etc. as a means of national survival beyond the means of national competitiveness. These are usually programs with high social impact but low short-term economic impact or large scientific programs that are too expensive and risky for private sector investment alone. The Republic of Korea has also shown a very successful model of economic progress and social development through government R&D programs. However, there have been many corruption scandals behind it while selecting awardees for government R&D programs in Korea. So, the Republic of Korea focused on reforming appraisal system for government R&D and began preparation for "Clean Appraisal System" last year. In this study, first we analyzed the related appraisal tasks through the review of laws and administrative rules and typed appraisal tasks according to the flow of the actors and time. Thus securing the information infrastructure and finally we drew the conceptual model of the system according to an open appraisal tasks by introducing an element of the OECD on open government typed appraisal tasks.

A method for selecting the evaluation index of defence R&D project by AHP (계층분석법에 의한 국방연구개발 평가지표 선정에 관한 연구)

  • Park, Seong;Hong, Yeon-Woong;Na, Joong-Kyung
    • Journal of the Korean Data and Information Science Society
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    • 제23권5호
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    • pp.961-970
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    • 2012
  • To evaluate companies that participated in the defense R&D project, 27 variables are chosen through literature survey, feature analysis of defense R&D and interviews with military experts. 17 variables are selected after factor analysis which is applied to reduce the number of variables and to detect structure in the relationships among variables, that is to classify variables using Likert-type scales. And then 17 variables are prioritized by AHP (analytic hierarchy process) method. It is shown that communication skill & cooperation strategy, level of technology, possession of needs technology have high priorities. However, protection plan of technology leakage, expertise of subcontractors, software development plan have low priorities.

Synthesis and Crystallization of Hydrazinium Nitroformate(HNF) as Eco-friendly Oxidizer (친환경 산화제 HNF 합성 및 결정화 연구)

  • Kim, Jina;Kim, Min Jun;Min, Byoung Sun
    • Journal of the Korean Society of Propulsion Engineers
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    • 제19권4호
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    • pp.69-76
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    • 2015
  • Recently, environmental sustainability of the transitional explosives and propellants is an issue of growing importance in energetic materials. For examples, ammonium perchlorate(AP) as an solid propellants oxidizer could create a poisonous gas and atmospheric pollutions, such as HCl. Among the several oxidizers, hydrazinium nitroformate(HNF) is an effective candidate substance for eco-friendly oxidizer, which has high density, pressure index, and less smog generating property during combustion for the Divert and Attitude Control System(DACS). This study was confirmed a synthesis through various conditions, was performed for the essential data of solubility the crystallization process. Also, crystallization process such as cooling, drowning-out and sonication were performed.

Development of Test Stand for Altitude Test of Reciprocating Engine (왕복동 엔진의 고도성능시험을 위한 시험장치 개발)

  • Lee, Kyung-Jae;Yang, Inyoung;Kim, Chun Taek;Kim, Dongsik;Baek, Cheulwoo;Yang, Gyaebyung
    • Journal of the Korean Society of Propulsion Engineers
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    • 제22권3호
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    • pp.119-127
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    • 2018
  • A test stand for an altitude test of reciprocating engine was designed, manufactured and validated by preliminary tests and simple calculations. The test stand was designed to interface with the altitude turbo-shaft engine test facility of Korea Aerospace Research Institute. Many limiting conditions for altitude test of reciprocating engine were assumed and the test stand was developed to satisfy these limitations. The test stand design was focused especially on the altitude, Mach number and fuel temperature control for reciprocating engine altitude tests with smaller air and fuel flow than those of turbo shaft engines.