• 제목/요약/키워드: launching

검색결과 759건 처리시간 0.023초

Ray-Launching 기법을 이용한 2.6 GHz 대역의 터널 내 경로손실 특성 분석 (Path Loss Characterization in Tunnel Using Ray Launching Method at 2.6 GHz)

  • 김도윤;조한신;육종관;박한규
    • 한국전자파학회:학술대회논문집
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    • 한국전자파학회 2003년도 종합학술발표회 논문집 Vol.13 No.1
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    • pp.33-37
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    • 2003
  • This paper presents the characteristics of large-scale fading in a tunnel environment. The Ray-Launching Method has been used to analyze the characteristics of the tunnel. For a curved tunnel, The concept of RDN (Ray Density Normalization) is introduced in order to obtain more accurate results. For our purposes, the structure of tunnel is assumed to be either a straight or curved tunnel having rectangular cross-section. A large scale fading has been presented shown in several tunnel cases.

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발사국의 개념재고 (The Concept of the 'Launching State' Revisited)

  • Aoki, Setsuko
    • 항공우주정책ㆍ법학회지
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    • 제15권
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    • pp.123-145
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    • 2002
  • Commercialization and privatization of outer space has been developing to the extent that public space law regime established at the UN seems to be somewhat incompatible with the today' s commercial launching services. Thus, this paper analyzes, at first, the UN space treaties to specify the obstacles for promoting commercial use. The necessity of some covert amendment of UN treaties is suggested through the national space legislation. Then three state practices are examined to propose a new concept of the "launching state" including the Sea Launch project, since the concept of the "launching state" is of the major importance to enact an effective national act to better accommodate UN space treaties to the present necessity.

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New Launching Concept for Free-Fall Lifeboats and Validation by Model Experiments and Numerical Simulations

  • Arai, Makoto
    • Journal of Ship and Ocean Technology
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    • 제6권1호
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    • pp.1-15
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    • 2002
  • A new concept for launching free-fall lifeboats, proposed by Yokohama National University is described in this paper. It has been pointed out that, using the conventional single-skid free-fall system, the potential for dangerous lifeboat motions (in which the lifeboat moves backward or jerks on the surface after entering the water) increases with the fall height of the lifeboat. One of the principal causes of this undesirable motion is vertical rotation of the lifeboat during its restricted fall at the edge of the launching skid. Thus a new "double-skid"launching concept is proposed to effectively eliminate the rotation of the lifeboat at the skid end and to enable the lifeboat to move smoothly after entering the water. In order to evaluate the performance of the proposed method, a series of model experiments and numerical simulations is carried out in which two lifeboat models with overall lengths of 1 meter and 6 meters are used. The effects of design parameters such as skid angle and skid height are investigated, and an example of the implementation of this new system at the stern of a large merchant ship is illustrated.

초음속 공중발사로켓의 임무형상 최적설계 (Optimal Mission Design of the Supersonic Air-launching Rocket)

  • 최영창;이재우;변영환
    • 시스템엔지니어링학술지
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    • 제1권1호
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    • pp.67-72
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    • 2005
  • Design and optimization study has been performed to obtain a supersonic air.launching mission for the nanosat launcher. Given mission is to launch 10kg payload to target orbit of $700km{\times}700km$. Additional design constraints are imposed by the mother plane. After the required velocity is obtained, the stag ing optimization is carried out. Serial analyses for the propulsion system and aerodynamics are performed then, the rocket trajectory optimization has been carried out. After several mission design and optimization iterations, the optimized mission which satisfies the mission target is obtained. Total weight of the three-staged air-launching rocket is 1231.4kg and the payload weight is 10 kg.

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1자유도 모델을 사용한 발사반발력 해석에 관한 연구 (A Study on the Analysis of the Rebounding Force using the 1-DOF Model)

  • 이종주;김좌일;김재호;함일배
    • 한국군사과학기술학회지
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    • 제15권4호
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    • pp.398-403
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    • 2012
  • This paper describes about the analysis of firing rebounding force exerted on the launching system supporting structure. The measured high pressure data at the launching tube is used as external force. The maximum firing rebounding force was occurred when the snubber of inner structure contacts the surface of wall in launching tube.

이중합성 연속 박스거더교에 대한 가설공법별 발생 단면력 검토 (Temporary Stresses by Applying Construction Methods for Continuous Steel-Concrete Double Composite Box Girder Bridges)

  • 최항용;서석구;오명석;오세환;김희성
    • 한국강구조학회 논문집
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    • 제19권6호
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    • pp.681-693
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    • 2007
  • 본 연구에서는 연속거더교량에 적용되고 있는 가설공법을 이중합성 박스거더교에 적용하여 발생 단면력을 검토하고, 적용성 측면에서 개선사항을 도출하고자 하였다. 하부콘크리트의 타설높이 및 타설범위는 각각 이중합성단면에 대한 소성모멘트 및 부모멘트영역에 의하여 결정되었다. 검토 가설공법은 일반적인 가설조건을 고려하여 크레인 가설공법, 켄틸레버 가설공법, 압출가설공법 등을 대상으로 하였으며, 이중합성 박스거더 가설 전의 하부콘크리트 타설유무에 따라 두가지의 경우로 구분하여 각각 시공중에 발생하는 단면력을 검토하였다. 또한, 압출가설공법 적용시의 단면력 저감방안으로 압출노즈에 의한 가설방안을 검토하였으며, 가설거더에 대한 압출노즈의 길이비, 단위중량비, 휨강성비 등의 변화에 따른 단면력의 저감정도를 검토하였다. 압출노즈에 의한 가설공법은 이중합성 박스거더교량에도 유효하게 적용될 수 있음을 확인하였다.

우주활동에 의하여 발생한 손해배상책임에 관한 연구 - 관련 사례를 중심으로 - (A Study on the Liability for Damage caused by Space Activity - With reference to Relevant Cases -)

  • 이강빈
    • 항공우주정책ㆍ법학회지
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    • 제26권1호
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    • pp.177-213
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    • 2011
  • 현재 우주활동에 의하여 발생된 손해에 대한 배상책임과 관련된 국제조약으로 1967년 우주조약과 1972년 우주손해배상책임조약이 있으며, 또한 우리나라 국내법으로 2008년 우주손해배상법이 있다. 우주조약은 우주활동에 대한 국가의 국제적 책임과 우주물체에 의한 손해에 대한 국가의 불법행위 책임에 관하여 규정하고 있다. 우주손해책임조약은 발사국의 절대적 책임, 과실책임, 연대책임, 배상청구권자, 배상청구방법, 배상청구기한, 배상청구와 국내적 구제, 손해배상액, 청구위원회 설치 등에 관하여 규정하고 있다. 우리나라 우주손해배상법은 우주손해의 정의, 우주손해책임조약과의 관계, 발사자의 무과실책임 및 책임의 집중, 발사자의 손해배상책임한도액, 발사자의 책임보험 가입, 정부의 피해자 구조 및 발사자 지원 등에 관하여 규정하고 있다. 우주사고로 인한 손해배상책임 관련 사례들로 Iridium33과 Cosmos 2251 위성충돌 사건, Cosmos 954 위성추락 사건, Martin Marietta의 위성발사 실패 사건, Westar VI 위성 작동불량 사고 등이 있으며, 이러한 우주사건에 관한 분쟁 또는 소송에 있어서 위성의 발사국, 발사자 및 제조자의 손해배상책임 부담문제에 관련하여 절대책임(엄격책임)원칙 또는 과실책임원칙이 적용되어 해결되고 있다. 우주손해책임조약의 개선방안으로 손해배상청구권자의 명확한 규정, 청구위원회의 결정의 구속력 확보 등을 들 수 있고, 우리나라 우주손해배상법의 개선방안으로 손해배상범위에 간접손해 포함, 손해배상책임 한도액의 통화단위 변경, 공동발사자의 연대책임 및 구상권 신설, 우주손해배상심의위원회의 설치 등을 들 수 있다. 우리나라는 2009년 6월 전남 고흥군 외나로도에 우주센터가 준공되어 동년 8월 및 2010년 6월 우리나라 최초 소형 우주발사체 나로호(KSLV-1)를 두차례 발사하였다. 향후 우리나라는 우주활동 과정에서 우주관련 국제조약 및 국내법상의 국제적 책임 및 우주손해에 대한 배상책임 등 문제들이 발생할 가능성이 있으므로 우리정부 및 우주물체 발사기관은 이러한 문제들에 대한 법적 제도적 대응책을 마련해야 할 것이다.

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우주손해배상법에 관한 약간의 고찰 (The compensation for damage by space accidents)

  • 김선이
    • 항공우주정책ㆍ법학회지
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    • 제22권2호
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    • pp.3-25
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    • 2007
  • In 2002 Republic of Korea successfully launched a self-made mined proportion rocket and it is expected that she will be able to have own space launching system by 2010. According to Article 14 of the Space Exploration Promotion Act, a new law should be established to impose the limit of compensation for the damage by space accident. Therefore, The Space Accident Liability Act was passed in Korean Congress on Nov. 22, 2007 and it will be enforced in six months. The purpose of this Act is to provide reparation for the damage of the third parties that a launch causes; and the Commonwealth should be insured against any possible space accidents to pay for such a damage. Here space accident means the damages to our life, body, and properties from the launching of space objects. There should be an actual loss to establish the compensation of Liability Act. Article 2 in Liability Act defines "damage" as follows: the term "damage" means loss of life, personal injury or loss of or damage to property of persons. Physical and material damages are included in the conception of damage. The meaning of a launching includes any test launch and launch for a real arrangement which will ultimately provides a wide range of compensation. Article 4 indicates that absolute liability should be imposed in compensating for damage by space accidents. Article 4 also indicates that a launching party should be absolutely liable to compensate for the damage caused by its space object on the surface of the Earth. In general, liability stands where fault is. But if the activity is ultra-hazardous and causes serious harm, the individual needs to compensate for the damage unlimitedly. Because of the many launchings for the Seattleite launching, a launching organization is obligated to the liability insurance in preparation for the space accidents. According to the Article 6 of Space Accident Liability Act, to be insured for the compensation for damage is obligatory. It says: "In accordance with Article 11 in the Space Exploration Promotion Act, the person who wants to receive an approval f3r launching needs to be insured in compensation for the possible damage by space accidents.

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우주법상 손해배상책임과 분쟁해결제도 (The Liability for Damage and Dispute Settlement Mechanism under the Space Law)

  • 이강빈
    • 한국중재학회지:중재연구
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    • 제20권2호
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    • pp.173-198
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    • 2010
  • The purpose of this paper is to research on the liability for the space damage and the settlement of the dispute with reference to the space activity under the international space treaty and national space law of Korea. The United Nations has adopted five treaties relating to the space activity as follows: The Outer Space Treaty of 1967, the Rescue and Return Agreement of 1968, the Liability Convention of 1972, the Registration Convention of 1974, and the Moon Treaty of 1979. All five treaties have come into force. Korea has ratified above four treaties except the Moon Treaty. Korea has enacted three national legislations relating to space development as follows: Aerospace Industry Development Promotion Act of 1987, Outer Space Development Promotion Act of 2005, Outer Space Damage Compensation Act of 2008. The Outer Space Treaty of 1967 regulates the international responsibility for national activities in outer space, the national tort liability for damage by space launching object, the national measures for dispute prevention and international consultation in the exploration and use of outer space, the joint resolution of practical questions by international inter-governmental organizations in the exploration and use of outer space. The Liability Convention of 1972 regulates the absolute liability by a launching state, the faulty liability by a launching state, the joint and several liability by a launching state, the person claiming for compensation, the claim method for compensation, the claim period of compensation, the claim for compensation and local remedy, the compensation amount for damage by a launching state, the establishment of the Claims Commission. The Outer Space Damage Compensation Act of 2008 in Korea regulates the definition of space damage, the relation of the Outer Space Damage Compensation Act and the international treaty, the non-faulty liability for damage by a launching person, the concentration of liability and recourse by a launching person, the exclusion of application of the Product Liability Act, the limit amount of the liability for damage by a launching person, the cover of the liability insurance by a launching person, the measures and assistance by the government in case of occurring the space damage, the exercise period of the claim right of compensation for damage. The Liability Convention of 1972 should be improved as follows: the problem in respect of the claimer of compensation for damage, the problem in respect of the efficiency of decision by the Claims Commission. The Outer Space Damage Compensation Act of 2008 in Korea should be improved as follows: the inclusion of indirect damage into the definition of space damage, the change of currency unit of the limit amount of liability for damage, the establishment of joint and several liability and recourse right for damage by space joint launching person, the establishment of the Space Damage Compensation Review Commission. The 1998 Final Draft Convention on the Settlement of Disputes Related to Space Activities of 1998 by ILA regulates the binding procedure and non-binding settlement procedure for the disputes in respect of space activity. The non-binding procedure regulates the negotiation or the peaceful means and compromise for dispute settlement. The binding procedure regulates the choice of a means among the following means: International Space Law Court if it will be established, International Court of Justice, and Arbitration Court. The above final Draft Convention by ILA will be a model for the innovative development in respect of the peaceful settlement of disputes with reference to space activity and will be useful for establishing the frame of practicable dispute settlement. Korea has built the space center at Oinarodo, Goheung Province in June 2009. Korea has launched the first small launch vehicle KSLV-1 at the Naro Space Center in August 2009 and June 2010. In Korea, it will be the possibility to be occurred the problems relating to the international responsibility and dispute settlement, and the liability for space damage in the course of space activity. Accordingly the Korean government and launching organization should make the legal and systematic policy to cope with such problems.

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