• Title/Summary/Keyword: 달탐사위성

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Mathematical Prediction of the Lunar Surface Temperature Using the Lumped System Analysis Method (집중계 해석법을 이용한 달 표면온도 예측)

  • Kim, Taig Young;Lee, Jang-Joon;Chang, Su-Young;Kim, Jung-Hoon;Hyun, Bum-Seok;Cheon, Hyeong Yul;Hua, Hang-Pal
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.4
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    • pp.338-344
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    • 2018
  • The lunar surface temperature is important as a environmental parameter for the thermal design of the lunar exploration vehicles such as orbital spacecraft, lander, and rovers. In this study, the temperature is numerically predicted through a simplified lumped system model for the energy conservation. The physical values required for the analysis of the energy equation are derived by considering the geometric shape, and the values presented in the previous research results. The areal specific heat, which is the most important thermo-physical property of the lumped system model, was extracted from the temperature measurements by the Diviner loaded on the LRO, and the value was predicted by calibration of the analytical model to the measurements. The predicted temperature distribution obtained through numerical integration has sufficient accuracy to be applied to the thermal design of the lunar exploration vehicles.

Development of KAMG engineering model in KPLO mission

  • Jin, Ho;Kim, Khan-Hyuk;Son, Derac;Lee, Seongwhan
    • The Bulletin of The Korean Astronomical Society
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    • v.43 no.1
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    • pp.48.4-48.4
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    • 2018
  • 대한민국 달탐사 시험용 궤도선은 2020년 말에 발사를 예정으로 위성개발이 진행되고 있다. KPLO(Korea Pathfinder Lunar Orbiter) 라고 명명된 달 궤도선에는 6개의 탑재체가 있으며, 경희대학교 우주탐사학과에서는 달 주위 공간 및 달 표면의 이상 자기장 영역을 관측하는 탑재체 (KMAG: Kplo MAGnetometer)를 개발하고 있다. 자기장센서는 3축 플럭스게이트 센서를 사용하며 약 0.2nT 이하의 분해능을 가지고 있다. 측정주기는 10Hz이며 총 무게는 3.5kg 이다. 1.2m 길이의 붐(Boom) 구조물 내부에 3개의 자기장 센서들을 설치하였으며 가능한 위성체로부터 거리를 두고 자기장을 측정하는 구조로 구성하였다. 시험모델 개발을 완료하고, 개발된 탑제체의 환경시험결과와 성능시험결과 요구조건에 부합되는 결과를 얻었다. KAMG는 국내최초의 심우주 탐사용 자기장 측정기로서 향 후, 행성 및 소행성 탐사 등에 활용하기 위한 기반 기술로 활용할 수 있을 것으로 기대한다.

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Radarsat-1 ScanSAR Quick-look Signal Processing and Demonstration Using SPECAN Algorithm (SPECAN 알고리즘을 이용한 Radatsat-1 ScanSAR Quick-look 신호 처리 및 검증 알고리즘 구현)

  • Song, Jung-Hwan;Lee, Woo-Kyung;Kim, Dong-Hyun
    • Korean Journal of Remote Sensing
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    • v.26 no.2
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    • pp.75-86
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    • 2010
  • As the performance of the spaceborne SAR has been dramatically enhanced and demonstrated through advanced missions such as TerraSAR and LRO(Lunar Reconnaissance Orbiter), the need for highly sophisticated and efficient SAR processor is also highlighted. In Korea, the activity of SAR researches has been mainly concerned with SAR image applications and the current SAR raw data studies are mostly limited to stripmap mode cases. The first Korean spaceborne SAR is scheduled to be operational from 2010 and expected to deliver vast amount of SAR raw data acquired from multiple operational scenarios including ScanSAR mode. Hence there will be an increasing demand to implement ground processing systems that enable to analyze the acquired ScanSAR data and generate corresponding images. In this paper, we have developed an efficient ScanSAR processor that can be directly applied to spaceborne ScanSAR mode data. The SPECAN(Spectrum Analysis) algorithm is employed for this purpose and its performance is verified through RADARSAT-1 ScanSAR raw data taken over Korean peninsular. An efficient quick-look processing is carried out to produce a wide-swath SAR image and compared with the conventional RDA processing case.

Conceptual Design of a Launch Vehicle for Lunar Exploration by Combining Naro-1 and KSLV-II (나로호와 한국형발사체를 연계한 달탐사 발사체 개념설계)

  • Yang, Won-Seok;Kim, So-Yeon;Choi, Jeong-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.8
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    • pp.654-660
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    • 2014
  • In this paper, a conceptual design of a launch vehicles is proposed by combining Naro-1 and KSLV-II. For trans-lunar injection (TLI) to lunar orbit at 300 km LEO, the target performance is defined same as that of KSLV-II, which delivers an object of 2.6 tons into 300 km LEO. The proposal launch vehicle concept of this study is combination of 1st stage of KSLV-I and 2-3rd stage of KSLV-II. Thus, it is possible to reduce the development time and also could expand the options for national launch vehicle capabilities with proven technologies.

275 GHz 이상 전파천문대역과 관련된 APG-11 2차 회의 결과

  • Chung, Hyun-Soo;Je, Do-Heung;Oh, Se-Jin;Roh, Duk-Gyoo;Sohn, Bong-Won;Lee, Sang-Sung;Kim, Hyo-Ryoung
    • The Bulletin of The Korean Astronomical Society
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    • v.35 no.1
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    • pp.46.1-46.1
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    • 2010
  • APT(Asian-Pacific Telecommunity)는 아시아-태평양지역 국가의 공동이익을 도모하기 위하여 결성된 아-태지역 전파협의체 조직으로, WRC(세계전파통신회의)회의에서의 아-태지역 주관청의 공동이익을 얻기 위해 APG(APT Conference Preparatory Group for WRC)회의를 연간 1회의 비율로 개최하고 있다. WRC-12회의에 대비하여 결성된 APG-12 회의가 2010년 3월 태국 방콕에서 개최되었으며, 전파천문업무 보호 및 22 GHz 대역 달탐사, 38 GHz 대역 Space-VLBI운용대역과 관련된 WRC-12 의제 1.6, 1.11, 1.12 등에 대해 활발한 토론이 있었다. WRC-12 의제 1.6은 수동업무(전파천문업무, 지구탐사위성 및 우주연구업무)를 능동업무의 유해혼신으로부터 보호하기 위하여 제정한 전파규칙 각주 5.565조의 개정 검토와 관련된 의제이다. 따라서 한국천문연구원에서는 275 GHz 이상 대역에서의 전파천문업무의 원활한 운용을 위해, WRC회의에서 최종적인 규정개정을 함에 있어서 필요한 아-태지역 국가의 공동의견을 창출하기 위한 APT회의에서 주도적인 역할을 담당하고 있다. 본 발표에서는 APG-12 3차 회의에 제출한 우리나라의 기고서 제출 결과 및 동 회의에서의 최종결과 및 향후 대응책에 대해서도 알아보고자 한다.

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275 GHz 이상 전파천문대역 보호를 위한 APG-12 5차회의 최종결과

  • Chung, Hyun-Soo;Je, Do-Heung;Oh, Se-Jin;Roh, Duk-Gyoo;Sohn, Bong-Won;Lee, Sang-Sung;Kim, Hyo-Ryoung
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.134.1-134.1
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    • 2011
  • APT(Asian-Pacific Telecommunity)는 아시아-태평양지역 국가의 공동이익을 도모하기 위하여 결성된 아-태지역 전파협의체 조직으로, WRC(세계전파통신회의)회의에서의 아-태 지역 주관청의 공동이익을 얻기 위해 APG(APT Conference Preparatory Group for WRC)회의를 연간 1회의 비율로 개최하고 있다. 2012년의 WRC-12회의에 대비하여 아태지역 회원국의 최종 공동의견서를 작성하기 위해, APG-12 5차회의가 2011년 8월 29일-9월 3일 부산에서 개최되었으며, 전파천문업무 보호 및 22 GHz 대역 달탐사, 38 GHz 대역 Space-VLBI운용대역과 관련된 WRC-12 의제 1.6, 1.11, 1.12 등에 대한 회의가 있었다. WRC-12 의제 1.6은 수동업무(전파천문업무, 지구탐사위성 및 우주연구업무)를 능동업무의 유해혼신으로부터 보호하기 위하여 제정한 전파규칙 각주 5.565조의 개정 검토와 관련된 의제이다. 따라서 한국천문연구원에서는 275 GHz 이상 대역에서 전파천문업무의 원활한 운용을 위해, APG-12 5차회의에 참석하여 WRC-12회의에 제출하기 위한 아-태지역 국가의 공동의견서 작성에 주도적인 역할을 담당하였다. 본 발표에서는 APG-12 5차 회의에 제안한 우리나라의 기고서 제안 내용 및 동 회의에서 의 최종 아태지역 회원국 공동의견서 결과 및 향후 대응책에 대해서도 알아보고자 한다.

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Suggestion of Korea's Deep Space Exploration Roadmap through Participation to the Artemis International Manned Lunar Exploration Program (한국의 Artemis 국제공동 유인달탐사 참여를 중심으로 우리나라 심우주탐사 로드맵 제안)

  • Choi, Gi-Hyuk;Kim, Dae-Yeong
    • Journal of Space Technology and Applications
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    • v.2 no.1
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    • pp.52-65
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    • 2022
  • Korea is near close the success on the indigenous launch vehicle KSLV-2 after the second test launch during the second half of 2022, and the satellite development has been already in the level of advanced country. After the such mature of satellite and launch vehicle technologies, Korea's space development main theme should be 'Space Exploration and Space Application', and paradigm should be changed from 'Hardware' to 'Scientific/Technological Mission', from 'Unmanned' to 'Manned'. Korea's prime space strategy should be the direction of expansion of space industry, creation of employment and secure the key technologies, improvement of convenience and safety of people. For the purpose it is necessary to start 'Manned Space Development' such that participation to 'Artemis and Gateway Program' in 20s' and manned Mars exploration in 30s' which would be carried out by means of global international cooperation, and which could be a good opportunity to explore the new area of space development and upgrade national technology capability. Taking advantage of this opportunity, it is required for Korea to join the international programs through developing indigenous challenging, sustainable Korean mission and hardware. Also selection of the 2nd Korean Astronaut could draw national attention, especially could give dreams to young generation. Participation to the Artemis program could be the opportunity of entering the major space fairing nation and boosting up national pride. In this study we survey and analyze the Artemis Program in detail, and in conclusion we suggest the strategy of Korea's participation to the Artemis Program.

Current Status of Nanotechnology Development for Space Exploration (우주탐사용 나노기술 개발 동향)

  • Lee, Ho-Sung;Chae, Yeon-Seok
    • Current Industrial and Technological Trends in Aerospace
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    • v.6 no.1
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    • pp.90-98
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    • 2008
  • Nanotechnology(NT) refers to a field of advanced micro-technology covering the creation and manufacturing of materials on the atomic and molecular scale and requires interdisciplinary study with various fields including materials science, physics, chemistry, electronics and others. Whileas nanotechnology is a kind of micro and small scaled science, space technology(ST) is one of the larger and system technologies utilizing broad fields of mechanical, materials, electronics and communication technologies. It is necessary to select and concentrate the functional items of nanotechnology for efficient application to be utilized in space technology, due to the cross-sectional characteristics of nanotechnology within nanomaterials, nanoelectronics, and nanomanufacturing. This paper provides the current state of art of nanotechnology in space technology by evaluating NASA's activities and the 9th frame of the project ANTARES(Analysis of Nanotechnology Applications in Space Developments and Systems) with the support of the German Aerospace Center (DLR), Space Flight Management, Division Technology for Space Systems and Robotics. It has shown that it is necessary to apply nanotechnology to space technology in order to achieve international competitiveness, for the nanotechnology can bring the previously impossible things to reality. Since KARI plans to send an unmanned probe to the moon's orbit and land a probe on the moon's surface in 2025, it is urgently needed to incorporate nanotechnology to national space development plan.

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