• Title/Summary/Keyword: Technologies for Aerospace

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우주파편 능동제거 기술 연구개발 동향 분석 (Recent Status on Active Space Debris Removal Technologies)

  • 김해동;김민기
    • 한국항공우주학회지
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    • 제43권9호
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    • pp.845-857
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    • 2015
  • 최근 우주쓰레기로 인한 우주환경 악화에 대한 국제적인 관심이 높아지고 있으며, 미국, 프랑스, 일본 등 우주개발 선진국들을 중심으로 우주파편 경감을 위한 가이드라인을 제정하여 준수하고자 노력하고 있는 추세이다. 이러한 노력과 더불어 우주파편을 직접 제거함으로써 그 숫자를 경감하고자 하는 기술을 '우주파편 능동제거 기술'이라고 한다. 본 논문에서는 우주파편 경감을 위한 해외 기관들의 연구동향과 배경들을 살펴보고 관련 기술개발 사례 및 특허들을 분석하였다. 또한, 이를 바탕으로 우주파편 능동제거시스템 개발을 위한 소요기술들을 분석해봄으로써 우리나라에서도 관련 연구에 관심을 가지고 본격적으로 시작하고자 하는 연구자들에게 선행연구 분석 자료로써 유용하게 활용될 수 있도록 하였다.

한국항공우주연구원의 가스터빈 엔진 핵심기술 개발현황 (Gas Turbine Core Technology Developments of Korea Aerospace Research Institute)

  • 김춘택;양인영
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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    • pp.277-278
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    • 2015
  • Korea Aerospace Research Institute(KARI) has developed the gas turbine core technologies since 1989 and has built the infrastructure for the development of gas turbine. Efficiency and flow instability are the major research object in radial and axial compressors. For combustor, NOx reduction is major research object. KARI also has developed turbine cooling technology as well as turbine aerodynamic technology.

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일본에서의 탄화규소장섬유세라믹스강화 복합재료 연구개발 (Recent Research Activities for Continuous SiC Fiber Reinforced Ceramic Matrix Composites in Japan)

  • 오가사와라 토시오
    • 세라미스트
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    • 제9권6호
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    • pp.18-23
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    • 2006
  • In this article, the present activities regarding research and development of continuous SiC fiber reinforced ceramic matrix composites (CFCC) in Japan are reviewed. The key technologies in SiC fiber composites are interphase between fiber and matrix and its oxidation resistance. To improve oxidation resistance of interphase, various kinds of technologies such as environment barrier coating, high dense matrix, unti-oxidation matrix, multi-layered intephase have been developed. It is suggested that high performance, affordable processing cost, and excellent reliability will be important factors to be in practical use of CMCs in future.

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Korea Pathfinder Lunar Orbiter (KPLO) Operation: From Design to Initial Results

  • Moon-Jin Jeon;Young-Ho Cho;Eunhyeuk Kim;Dong-Gyu Kim;Young-Joo Song;SeungBum Hong;Jonghee Bae;Jun Bang;Jo Ryeong Yim;Dae-Kwan Kim
    • Journal of Astronomy and Space Sciences
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    • 제41권1호
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    • pp.43-60
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    • 2024
  • Korea Pathfinder Lunar Orbiter (KPLO) is South Korea's first space exploration mission, developed by the Korea Aerospace Research Institute. It aims to develop technologies for lunar exploration, explore lunar science, and test new technologies. KPLO was launched on August 5, 2022, by a Falcon-9 launch vehicle from cape canaveral space force station (CCSFS) in the United States and placed on a ballistic lunar transfer (BLT) trajectory. A total of four trajectory correction maneuvers were performed during the approximately 4.5-month trans-lunar cruise phase to reach the Moon. Starting with the first lunar orbit insertion (LOI) maneuver on December 16, the spacecraft performed a total of three maneuvers before arriving at the lunar mission orbit, at an altitude of 100 kilometers, on December 27, 2022. After entering lunar orbit, the commissioning phase validated the operation of the mission mode, in which the payload is oriented toward the center of the Moon. After completing about one month of commissioning, normal mission operations began, and each payload successfully performed its planned mission. All of the spacecraft operations that KPLO performs from launch to normal operations were designed through the system operations design process. This includes operations that are automatically initiated post-separation from the launch vehicle, as well as those in lunar transfer orbit and lunar mission orbit. Key operational procedures such as the spacecraft's initial checkout, trajectory correction maneuvers, LOI, and commissioning were developed during the early operation preparation phase. These procedures were executed effectively during both the early and normal operation phases. The successful execution of these operations confirms the robust verification of the system operation.

큐브위성 STEP Cube Lab. 비행모델의 전자조립 및 기능시험 과정 (A Series of Process of Electrical Integration and Function Test for Flight Model of STEP Cube Lab.)

  • 정현모;채봉건;한상혁;오현웅
    • 한국항공우주학회지
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    • 제44권9호
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    • pp.814-824
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    • 2016
  • 본 논문에서 제안한 우주기반기술 검증용 큐브위성의 명칭은 STEP Cube Lab. (Cube Laboratory for Space Technology Experimental Project)으로 주요임무는 국내 산학연에서 기수행된 우주핵심기술을 발굴하며, 자체 개발 탑재체를 궤도 검증하는 것이다. 상기의 임무 구현을 위해 체계 레벨에서의 요구조건에 따라 전자조립 및 기능시험을 수행하였다. 또한, 비행 소프트웨어 설계의 유효성을 입증하였으며, 발사 궤도 열 환경시험을 통해 수락수준의 비행모델 검증을 완료하였다. 본 논문에서는 FM EIT, 발사 궤도 열 환경에서 수행한 기능시험의 일련 과정을 소개하고자 한다.

액체로켓 기반 2단형 소형발사체의 스테이징 및 임무설계 (Staging and Mission Design of a Two-Staged Small Launch Vehicle Based on the Liquid Rocket Engine Technology)

  • 서대반;이준성;이기주;박재성
    • 한국항공우주학회지
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    • 제50권4호
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    • pp.277-285
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    • 2022
  • 뉴스페이스 시대를 대표하는 소형위성 분야에서 발사기회에 대한 수요가 크게 증가하고 있다. 이를 위한 소형위성 전용 발사서비스를 합리적인 가격에 제공하는 것은 많은 스타트업 기업들이 추구하는 새로운 비즈니스 모델이 되고 있으며, 여기에는 저비용 부품과 대량생산, 최적화된 제작 공정이 결합된 비용 절감을 위한 혁신적인 솔루션들이 요구되고 있다. 이러한 흐름 속에서 우리나라에서도 한국항공우연구원에서 제3차 우주개발 진흥 기본계획에 따라 누리호를 통해 개발된 액체로켓엔진 기술을 기반으로 2단형 소형발사체 개발에 대비하여 핵심기술 및 비용절감 기술들을 개발하기 위한 선행기술 연구에 착수하였다. 본 논문에서는 소형위성을 위한 혁신적이며 가격 경쟁력을 가지는 것을 목표로 하는 2단형 소형발사체의 개념을 소개하고, 스테이징 설계 및 2단형 발사체의 전기체 구성안을 포함한 임무설계 결과를 기술하였다.

항공보안장비 성능인증제의 고도화 방안에 관한 연구 (Aviation Security Equipments Certification System in Korea: Suggestions for Improvement)

  • 이원주;유상우;박수홍;김경훈;하다솜;설은숙;한수진;박서하;이지수;김찬휘;강진구;이기영
    • 품질경영학회지
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    • 제48권3호
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    • pp.395-408
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    • 2020
  • Purpose: This study was performed for advancement of aviation security equipments certification system. Methods: We investigated aviation security equipments certification-related registrations and the latest research trends of explosive detection technologies. Based on the literature studies, we draw the critical issues of the aviation security equipment certification system and suggested improvement direction. Results: We found some inaccuracies of the definition of explosive trace detection equipments, accreditation review committee, and performance evaluation test method. These problems should be modified to suit being practical. Conclusion: The present results would be useful for basic data for modifying aviation security equipments certification systems.

Urban Spatial Analysis using Multi-temporal KOMPSAT-1 EOC Imagery

  • Kim Youn-Soo;Jeun Gab-Ho;Lee Kwang-Jae;Kim Byung-Kyo
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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    • pp.515-517
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    • 2004
  • Although sustainable development of a city should in theory be based on updated spatial information like land cover/use changes, in practice there are no effective tools to get such information. However the development of satellite and sensor technologies has increased the supply of high resolution satellite data, allowing cost-effective, multi-temporal monitoring. Especially KOMPSAT-1(KOrea Multi-Purpose SATellite) acquired a large number of images of the whole Korean peninsula and covering some large cities a number of times. In this study land-use patterns and trends of Daejeon from the year 2000 to the year 2003 will be considered using land use maps which are generated by manual interpretation of multi-temporal KOMPSAT EOC imagery and to show the possibility of using high resolution satellite remote sensing data for urban analysis.

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