• Title/Summary/Keyword: 우주 추진

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중형항공기사업의 새로운 장 마련할 AI(R) 프로젝트

  • 한국항공우주산업진흥협회
    • Aerospace Industry
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    • v.50
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    • pp.18-21
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    • 1997
  • 표류하던 중형항공기사업에 새바람이 불었다. 중국과의 협상결렬과 포커사의 인수불발로 답보상태에 빠져있던 중형기사업조합은 그동안 대안사업을 추진한 결과 지난 97년 4월 11일 유럽의 지역간 항공기 제작업체인AI(R)사와 항공기국제공동개발에 대한 양해각서(MOU)를 체결하고 올 하반기부터 본격적으로 사업을 추진키로 했다. 본 고에는 그동안 AI(R)사의 선정과정과 배경 그리고 협상내용을 살펴보기로 한다.

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Development of Chemical and Electric Propulsion Systems for Spacecraft in UK (영국의 우주비행체용 화학추진 및 전기추진시스템 개발)

  • HAN, Cho Young
    • Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.37-45
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    • 2008
  • KARI has jointly developed COMS bipropellant propulsion system with EADS Astrium, UK. It is well known at the moment about American or even German efforts for space development and space propulsion activities. On the contrary UK's capability for space development hasn't been recognised well in Korea. The major space activities relevant to the development of chemical and electric propulsion systems in UK, in reference to our space propulsion programme are addressed in detail. In addition the collaboration in prospect between two countries is proposed.

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항공산업 발전비전과 세부 추진전략

  • 한국항공우주산업진흥협회
    • Aerospace Industry
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    • v.79
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    • pp.4-9
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    • 2002
  • 지난 7월말 산업자원부와 경제5단체는 세계 4강 실현전략을 담은 ''''2010 산업비전과 발전전략: 산업 4강으로의 길''''을 확정, 발표한 바 있다. 이 보고서에서는 미래전략산업의 하나로 분류된 항공산업분야에서 2015년까지 헬기, 훈련기 수출국으로 도약, 세계 10위권 항공업체 육성과 우리나를 항공전자 등 주요 부품의 세계 공급기지로 발전시키겠다는 비전을 제시하고 있다. 다음은 ''''2010 산업비전과 발전전략''''에서 밝힌 항공산업의 발전 가능성 및 당면 문제점, 항공산업 발전비전, 과제별 세부 추진전략을 중심으로 정리했다.

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다목적실용위성 2호 위성본체 국산화 개발

  • Hwang, Do-Sun
    • Aerospace Industry
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    • v.84
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    • pp.10-15
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    • 2004
  • 인공위성 및 발사체 등의 우주산업은 21세기를 이끌어 갈 첨단기술 산업이며 국가 과학기술력의 척도로서 자리매김하고 있다. 우주개발 선진국인 미국인 영구 달기지 건설 및 유인 우주탐사 계획을 적극적으로 추진하고 있으며 중국도 미국, 러시아에 이어 유인 우주선을 발사한 세번째 국가가 되었다.<중략>

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산업 - 서울 국제 항공우주 및 방위산업 전시회 2009

  • 한국항공우주산업진흥협회
    • Aerospace Industry
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    • s.104
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    • pp.26-33
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    • 2009
  • "서울 국제 항공우주 및 방위산업 전시회 2009" 행사가 오는 10월 20일부터 25까지 6일간 서울공항(성남 소재)에서 개최될 예정이다. 1995년 첫 행사가 개최된 이래 격년으로 펼쳐지는 이번 전시회는 국내외 인사 및 민 관 군 주요 관계자들이 참석하며, 정부기관 및 자치단체에서 후원하는 범정부적인 행사로 추진 중이다.

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Technology Development Prospects and Direction of Reusable Launch Vehicles and Future Propulsion Systems (재사용 발사체 및 미래추진기관 기술발전 전망 및 방향)

  • Kim, Chun Taek;Yang, Inyoung;Lee, Kyungjae;Lee, Yangji
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.8
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    • pp.686-694
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    • 2016
  • During the Cold War, all space developments were focused on the performance only. However economy becomes more important for space development after the Cold War. There is a growing interest in reusable launch vehicle to secure the economic feasibility. In this paper, technology development prospects and direction of reusable launch vehicles and future propulsion systems of various countries are presented.

Risk Management of Launch Vehicle Propulsion System (우주 발사체 추진기관의 위험 관리)

  • Cho, Sang-Yeon;Shin, Myung-Ho;Ko, Jung-Hwan;Oh, Seung-Hyub;Park, Jeong-Joo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.3-6
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    • 2007
  • Korea Aerospce Research Institute(KARI) has been developing the first civilian rocket, Korea space launch vehicle (KSLV-I), which can put the small size satellite into designated orbit. Developing launch vehicles contains a lot of uncertainty due to large scale, complexity, and technical difficulty. The uncertainty may become risk in the areas of business and technology which causes schedule delay, cost increase, and design changes of subsystems and components. This study describes the technical risk identification methods using FTA and procedures of planning and implementation of risk assessment and reduction of launch vehicle propulsion system.

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Analysis of Inverter Losses according to Switching Frequency Using Electric Motor for Aircraft (스위칭 주파수에 따른 전기 추진 항공기용 인버터 손실 분석)

  • Koo, Bon-soo;Jo, Seong-hyeon;Choi, In-ho
    • Journal of Aerospace System Engineering
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    • v.15 no.1
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    • pp.32-39
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    • 2021
  • Electric propulsion aircraft are being actively researched in the aviation field in recent years to solve environmental and noise problems caused by existing gas turbine engine. In particular, research on a thrust motor as a core component of an electric power propulsion system and an inverter for driving it is actively being conducted. In this paper, a motor with high specific power is selected to determine characteristics of aircraft that are sensitive to weight and volume. Power loss of the inverter is then simulated. In the simulation, the selected motor and power device were modeled using PSIM, a power electronics analysis tool. Inverter power loss according to switching frequency was then analyzed.

Technical Heritage of UK Chemical Propulsion Systems and COMS Bipropellant Propulsion System (영국산 화학추진시스템의 기술이력과 통신해양기상위성 이원추진제 추진시스템)

  • HAN, Cho Young
    • Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.28-36
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    • 2008
  • The technology relevant to a bipropellant propulsion system is quite new one in Korea, which is being transferred for the first time, with development of COMS propulsion system. It hasn't ever attempted before, and hasn't got any general idea itself as well, in Korea. The technical heritage of UK bipropellant propulsion pertinent to COMS propulsion system is scrutinised mainly. Furthermore the strong possibility of COMS CPS for the moon explorer mission is rationalised on the basis of the history of successful predecessors.

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Study of Cold Gas Propulsion System Utilizing Butane as Liquefied Propellant (부탄을 액화 연료로 사용한 냉가스 추진 시스템에 대한 연구)

  • Kang, Suk-Jin;Kwon, Ky-Beom;Cho, Dong-Hyun;Lee, Sang-Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.4
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    • pp.323-328
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    • 2007
  • A direct application of liquefied gas propellants to a typical small satellite cold gas propulsion system was analyzed. Performance of systems using liquefied gas propellant under consideration was compared to that of a nitrogen cold gas propulsion system. Liquefied gas propellant propulsion system's performance, required tank volume, and required propulsion system mass has been calculated at the same mass, volume, and total impulse condition of a typical nitrogen cold gas propulsion system. It was found that the liquefied gas propulsion system has advantages in performance, volume, and mass, compared to a typical nitrogen cold gas system, and can be directly applied to a cold gas propulsion system.