• Title/Summary/Keyword: 우주환경보호

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원격제어 시스템

  • 손재범;정완균;염영일
    • ICROS
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    • v.2 no.3
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    • pp.42-60
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    • 1996
  • 이 글에서는 원격제어 시스템의 역사, 적용에서 이론까지 간략하게 다루어 보았다. 과학기술이 발달하고 생활수준이 향상됨에 따라 인간은 소위 3D 직종을 기피하려는 경향을 갖게 되었다. 또한 작업환경의 변화가 심하고 위험한 심해저나 원자력 발전소, 우주공간에서의 작업 등은 인간이 맡게 되면 엄청난 인건비가 소요되고, 작업자의 안전을 보장할 수가 없게 된다. 로봇을 이용하여 이러한 작업들을 대치하게 될 경우 무엇보다도 작업자를 보호할 수 있다는 장점이 있다. 그러나 순간적인 판단과 작업을 반복하거나 돌발적인 사고에 대처하는 능력이 로봇에게는 절대적으로 부족하기 때문에, 반대급부적으로 원격 제어 시스템의 가치가 점점 높아지고 있다. 원격 제어 시스템은 우주공간, 방사능 지역 등에서의 작업시 인간을 보호하고, 작업의 효율성 증대에 기여할 뿐만 아니라, 최근에 활발히 연구가 진행되고 있는 초정밀 로봇을 이용한 원격 수술(telesurgery)이나 사람이 들 수 없는 무게를 작업자의 의도대로 다룰 수 있게 하는 등 인간의 한계를 극복하는 데도 큰 몫을 담당할 것으로 기대되기 때문에 계속적인 연구를 필요로 하고 있다.

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A Comparative Study between Space Law and the Law of the Sea (우주법과 해양법의 비교 연구)

  • Kim, Han-Taek
    • The Korean Journal of Air & Space Law and Policy
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    • v.24 no.2
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    • pp.187-210
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    • 2009
  • Space law(or outer space law) and the law of the sea are branches of international law dealing with activities in geographical ares which do not or do only in part come under national sovereignty. Legal rules pertaining to the outer space and sea began to develop once activities emerged in those areas: amongst others, activities dealing with transportation, research, exploration, defense and exploitation. Naturally the law of the sea developed first, followed, early in the twentieth century, by air law, and later in the century by space law. Obviously the law of the sea, of the air and of outer space influence each other. Ideas have been borrowed from one field and applied to another. This article examines some analogies and differences between the outer space law and the law of the sea, especially from the perspective of the legal status, the exploration and exploitation of the natural resources and environment. As far as the comparisons of the legal status between the outer space and high seas are concerned the two areas are res extra commercium. The latter is res extra commercium based on both the customary international law and treaty, however, the former is different respectively according to the customary law and treaty. Under international customary law, whilst outer space constitutes res extra commercium, celestial bodies are res nullius. However as among contracting States of the 1967 Outer Space Treaty, both outer space and celestial bodies are declared res extra commercium. As for the comparisons of the exploration and exploitation of natural resources between the Moon including other celestial bodies in 1979 Moon Agreement and the deep sea bed in the 1982 United Nations Convention on the Law of the Sea, the both areas are the common heritage of mankind. The latter gives us very systematic models such as International Sea-bed Authority, however, the international regime for the former will be established as the exploitation of the natural resources of the celestial bodies other than the Earth is about to become feasible. Thus Moon Agreement could not impose a moratorium, but would merely permit orderly attempts to establish that such exploitation was in fact feasible and practicable, by allowing experimental beginnings and thereafter pilot operations. As Professor Carl Christol said until the parties of the Moon Agreement were able to put into operation the legal regime for the equitable sharing of benefits, they would remain free to disregard the Common Heritage of Mankind principle. Parties to one or both of the agreements would retain jurisdiction over national space activities. In so far as the comparisons of the protection of the environment between the outer space and sea is concerned the legal instruments for the latter are more systematically developed than the former. In the case of the former there are growing tendencies of concerning the environmental threats arising from space activities these days. There is no separate legal instrument to deal with those problems.

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Thermal Analysis of Exhaust Diffuser Cooling Channels for High Altitude Test of Rocket Engine (로켓엔진 고공환경 모사용 디퓨져의 냉각 채널 열 해석)

  • Cho, Kie-Joo;Kim, Yong-Wook;Kan, Sun-Il;Oh, Seung-Hyub
    • Aerospace Engineering and Technology
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    • v.9 no.2
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    • pp.193-197
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    • 2010
  • Water cooling ducts are installed in the exhaust diffuser for high altitude tests of rocket engine to protect diffuser from high-temperature combustion gas. The mass flow rate and pressure of cooling water is designed to prevent boiling of cooling water in the ducts. Therefore, the estimation of maximum temperature of duct wall is important parameter in design of cooling system, especially pressure of cooling water. The method for predicting maximum temperatures of duct walls with variation of coolant flow rates was derived theoretically.

The Problem of Space Debris and the Environmental Protection in Outer Space Law (우주폐기물과 지구 및 우주환경의 보호)

  • Lee, Young Jin
    • The Korean Journal of Air & Space Law and Policy
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    • v.29 no.2
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    • pp.205-237
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    • 2014
  • Last 50 years there were a lot of space subjects launched by space activities of many states and these activities also had created tremendous, significant space debris contaminating the environment of outer space. The large number of space debris which are surrounding the earth have the serious possibilities of destroying a satellite or causing huge threat to the space vehicles. For example, Chinese anti-satellite missile test was conducted by China on January 11, 2007. As a consequence a Chinese weather satellite was destroyed by a kinetic kill vehicle traveling with a speed of 8 km/s in the opposite direction. Anti-satellite missile tests like this,contribute to the formation of enormous orbital space debris which can remain in orbit for many years and could interfere with future space activity (Kessler Syndrome). The test is the largest recorded creation of space debris in history with at least 2,317 pieces of trackable size (golf ball size and larger) and an estimated 150,000 debris particles and more. Several nations responded negatively to the test and highlighted the serious consequences of engaging in the militarization of space. The timing and occasion aroused the suspicion of its demonstration of anti-satellite (ASAT) capabilities following the Chinese test of an ASAT system in 2007 destroying a satellite but creating significant space debris. Therefore this breakup seemed to serve as a momentum of the UN Space Debris Mitigation Guidelines and the background of the EU initiatives for the International Code of Conduct for Outer Space Activities. The UN Space Debris Mitigation Guidelines thus adopted contain many technical elements that all the States involved in the outer space activities are expected to observe to produce least space debris from the moment of design of their launchers and satellites until the end of satellite life. Although the norms are on the voluntary basis which is normal in the current international space law environment where any attempt to formulate binding international rules has to face opposition and sometimes unnecessary screening from many corners of numerous countries. Nevertheless, because of common concerns of space-faring countries, the Guidelines could be adopted smoothly and are believed faithfully followed by most countries. It is a rare success story of international cooperation in the area of outer space. The EU has proposed an International Code of Conduct for Outer Space Activities as a transparency and confidence-building measure. It is designed to enhance the safety, security and sustainability of activities in outer space. The purpose of the Code to reduce the space debris, to allow exchange of the information on the space activities, and to protect the space objects through safety and security. Of the space issues, the space debris reduction and the space traffic management require some urgent attention. But the current legal instruments of the outer space do not have any binding rules to be applied thereto despite the incresing activities on the outer space. We need to start somewhere sometime soon before it's too late with the chaotic situation. In this article, with a view point of this problem, focused on the the Chinese test of an ASAT system in 2007 destroying a satellite but creating significant space debris and tried to analyse the issues of space debris reduction.

정보통신부 전파방송관리국 2001년도 주요업무 계획

  • The Korea Society of Space Technology
    • Satellite Communications and Space Industry
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    • v.9 no.1 s.21
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    • pp.46-63
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    • 2001
  • 최근 들어 전파 이용은 기존의 이동전화.방송에서 교통, 의료, 과학, 치안 등 모든 분야로 확대되고, 다양한 전파응용기술이 발전하면서 무선국 수가 1990년 기준(22만 5천국)으로 1995년에는 10배, 2000년에는 100배를 상회하여 매 5년마다 10배씩 급격히 증가하고 있다. 이와 함께 국내 전파통신서비스 시장 또한 1990년 718억원에서 1999년 9조8천억원으로 연평균 70%이상 성장하였고, 전파산업의 GDP 비중 역시 1996년 3.5%에서 1999년 5.1%로 증가하는 등 국가 경제에서 전파산업의 비중이 급속히 확대되면서 전파는 국민 경제의 핵심요소로 등장하고 있다. 정통부 전파방송관리국은 전파통신 기반확충과 효율적 전파관리, 방송매체의 디지털화와 방송기술의 고도화, 전파.방송산업의 활성화 지원, 우주통신 개발촉진 및 이용의 활성화, 전파 환경 보호 및 전파이용질서의 확립 등을 2001년도 중점사업으로 하고 있다. 이에 전파방송관리국의 2001년 주요 업무계획 내용을 원문 그대로 게재한다.

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Design and Verification of Housing and Memory Board for Downsizing for Crash Protected Memory Module (충돌보호메모리모듈의 소형화를 위한 하우징 및 메모리 보드 설계와 검증)

  • Kim, Jun-Hyoung;Kim, Jung-Pil;Kim, Jeong-Yeol;Kim, Tae-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.1
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    • pp.81-88
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    • 2020
  • Flight data recorder is a equipment that records data required for investigation of aircraft accidents and should be developed in compliance with the ED-112A standard. Unlike general data storage device, flight data recorder must be able to recover data after an aircraft accident, requiring a housing and a memory board to protect data in extreme environments. To attain this performance, we designed a housing that can withstand the test by analyzing the physical environment of the impact, shear/tensile, penetration resistance and static crush test of the crash survival test and minimized the size and weight compared to the existing one in consideration of the installation of the aircraft in this paper. Insulation material and thermal block material were applied to endure high and low temperature fire so that the internal temperature does not rise above 150℃ even in 260℃, 10 hour environment. In addition, the memory board is designed to minimize the size and we devise a hoping programming method to prevent continuous data loss of more than 16 seconds. Through this, Crash protected memory module that satisfies ED-112A was completed.

달과 화성의 토양에서 지하 깊이에 따른 고에너지 우주선 환경 영향 분석

  • Jeong, Jong-Il;Son, Jong-Dae;Lee, Yu;O, Su-Yeon
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.104.2-104.2
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    • 2012
  • 미국, 중국, 일본, 인도 등과 같은 세계 여러 국가들이 달 및 화성 탐사를 수행하고 있는 현시점에서 우리나라도 2025년에 달 탐사를 계획하고 있다. 인간에게 있어서 우주공간은 고에너지 환경의 영향을 많이 받는 곳이다. 향후 달, 화성과 같은 다른 행성으로의 이주를 생각하고 있는 현 시점에서 우리는 고에너지우주방사선 환경의 영향을 고려해야 한다. 지구에서의 인간은 지구 자기장과 대기에 의해 고에너지 우주선 환경으로부터의 영향을 덜 받는다. 그러나 달과 화성의 경우는 다르다. 달의 대기는 거의 없고 자기장도 무시할 정도로 매우 작으며, 화성 또한 자기장이 거의 없으며 대기 또한 얇아서 Galactic Cosmic Ray (GCR)나 Solar Energetic Proton (SEP) 등으로부터 인간은 많은 영향을 받을 수 있다. 이러한 위험으로부터 인간이 보호받을 수 있는 곳은 달과 화성의 지표 아래나 동굴이라고 볼 수 있다. 그래서 달 및 화성의 표면과 지하 영역에 대한 고에너지 우주선 환경의 깊이에 따른 영향을 분석하여 어느 정도로 두터운 천장을 가진 동굴이어야 우주인들이 상주하는 지하공간을 지구표면에서의 방사선 환경과 같은 수준으로 유지할 수 있는지를 추정해 보려고 한다. 달 표면 토양의 화학적 구성성분은 Maria와 Highlands로 구분되어 약간의 차이가 있다. 달의 Maria 토양은 $SiO_2$ - 45.4%, $Al_2O_3$ - 14.9%, CaO - 11.8%, FeO - 14.1%, MgO - 9.2%, $TiO_2$ - 3.9%, $Na_2O$ - 0.6%이고 Highlands의 토양은 $SiO_2$ - 45.5%, $Al_2O_3$ - 24.0%, CaO - 15.9%, FeO - 5.9%, MgO - 7.5%, $TiO_2$ - 0.6%, $Na_2O$ - 0.6%의 화학적인 구성비를 가진다. 또한 화성표면은 $SiO_2$ - 43.9%, $Al_2O_3$ - 8.1%, CaO - 6.0%, FeO - 18.1%, MgO - 7.1%, $Na_2O$ - 1.4%의 토양의 화학적인 구성비를 가지고 있다. 본 연구에서는 이러한 구성비를 가지고 있는 달과 화성 표면에 대한 우주방사선의 영향을 분석하기 위해서 GEANT4를 사용하여 수행한 전산 모사의 결과를 발표할 것이다.

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A Study on Applying Zero Trust Architecture: Focusing on Implementing Remote Work System (제로 트러스트 아키텍처 적용 방안에 대한 연구: 재택근무 시스템 구성을 중심으로)

  • Jaewoo Do;Keumseok Kang
    • Journal of the Korea Institute of Information Security & Cryptology
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    • v.33 no.6
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    • pp.1001-1020
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    • 2023
  • As massive increase in remote work since COVID-19, the boundaries between the inside and outside of corporate networks have become blurred. As a result, traditional perimeter security has stagnated business productivity and made it difficult to manage risks such as information leakage. The zero trust architecture model has emerged, but it is difficult to apply to IT environments composed of various companies. Therefore, using the remote work system configuration as an example, we presented a configuration and methodology that can apply zero trust models even in various network environments such as on-premise, cloud, and network separation. Through this, we aim to contribute to the creation of a safe and convenient cyber environment by providing guidance to companies that want to apply zero trust architecture, an intelligent system that actively responds to cyber threats.

The Contents of SatDSiG and Its Implications for Korea (독일 위성자료보안법의 내용 및 시사점)

  • JUNG, Yungjin
    • Journal of Aerospace System Engineering
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    • v.13 no.2
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    • pp.60-65
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    • 2019
  • TerraSAR-X, launched in June 2007, and TanDEM-X, June 2010, are remote-sensing satellites with 1M resolution that are capable of observing the ground even during the nighttime and poor weather conditions. The two satellites had been developed under a public-private partnership between the German Aerospace Centre and Airbus in the interest of the commercial marketing for German satellite data. However, the data of high-grade earth remote-sensing system, such as those of the satellites, has been produced by a military satellite and thus used under limited circumstances in Germany. Therefore, a legislation to commercialize the German satellite data and to protect its national security is needed. For this, SatDSiG was enacted in December 2007. Thus this article will contain the main contents of SatDSiG and its implication for Korea, which stared to export data of Kompsat 3, 3A and 5 in 2018.

Thermomechanical Coupled Analysis of Carbon/phenolic Composite Structures in Reentry Environments (재진입 환경의 탄소/페놀릭 복합재 구조물의 열기계적 연계 해석)

  • Son, Myeong Jin;Shin, Eui Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.6
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    • pp.414-421
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    • 2019
  • In this paper, thermomechanical coupled analysis of carbon/phenolic composites structures in reentry environment was performed. The interface of thermomechanical coupled analysis was constructed using commercial software. The governing equations of temperature and displacement fields were considered to simulate change of physical behavior due to pyrolysis and ablation effects. The results of thermomechanical coupled analysis were compared with the results of ablation test using arc-heated wind tunnel. Also, the structural stability of reentry capsule was analyzed using the analysis interface. The excellent ablation characteristics and thermal protection effects of the carbon/phenolic composites were confirmed and the constructed analysis interface can be effectively used to perform thermal protection system design.