• Title/Summary/Keyword: Launch site

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A Design and Development of n Large Scale On-Line Game Server Based on PaaS (PaaS 기반 대규모 온라인 게임 서버 설계 및 구현)

  • Hur, Sung-Jin
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.9 no.4
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    • pp.1006-1011
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    • 2008
  • In this paper, we developed a system for large scale on-line interactive game server based on Platform as a Service(PaaS). Small and medium sized game developing companies have various aspects of limitation to launch a large scale on line game site. By using the system proposed in this paper, small and medium sized game developing companies can easily publish their games into market.

OVERVIEW OF KOREA OCEAN SATELLITE CENTER (KOSC) DEVELOPMENT

  • Yang, Chan-Su;Han, Hee-Jeong;Ahn, Yu-Hwan;Moon, Jeong-Eon;Lee, Nu-Ree
    • Proceedings of the KSRS Conference
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    • v.1
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    • pp.75-78
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    • 2006
  • The Korea Ocean Satellite Center (KOSC) is under development to establish in line with the launch of the first Korean multi-function geostationary satellite COMS (Communication, Ocean and Meteorological Satellite) scheduled in 2008. KOSC aims to receive, process and distribute Geostationary Ocean Color Sensor (GOCI) data on board COMS in near-real time. In this report, current status of KOSC development is presented in the following categories; site selection for KOSC, antenna design, GOCI data receiving and processing system, data distribution, future works.

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Design, Implementation, and Validation of KOMPSAT-2 Software Simulator

  • Lee, Sang-Uk;Lee, Byoung-Sun;Kim, Jae-Hoon;Cho, Sung-Ki
    • ETRI Journal
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    • v.27 no.2
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    • pp.140-152
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    • 2005
  • In this paper, we present design features, implementation, and validation of a satellite simulator subsystem for the Korea Multi-Purpose Satellite-2 (KOMPSAT-2). The satellite simulator subsystem is implemented on a personal computer to minimize costs and trouble on embedding onboard flight software into the simulator. An object-oriented design methodology is employed to maximize software reusability. Also, instead of a high-cost commercial database, XML is used for the manipulation of spacecraft characteristics data, telecommand, telemetry, and simulation data. The KOMPSAT-2 satellite simulator subsystem is validated by various simulations for autonomous onboard launch and early orbit phase operations, anomaly operation, and science fine mode operation. It is also officially verified by successfully passing various tests such as the satellite simulator subsystem test, mission control element system integration test, interface test, site installation test, and acceptance test.

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나로 우주센터 종합낙뢰감지시스템 소개 및 기술동향

  • Kim, Hong-Il;Choe, Mi-Yeon;Guk, Bong-Jae
    • Current Industrial and Technological Trends in Aerospace
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    • v.4 no.2
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    • pp.49-54
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    • 2006
  • 현재 전라남도 고흥 외나로도에서는 발사체를 발사하기 위한 우주센터를 건립 중에 있다. 우주센터 내에는 추적레이다, 발사대, 발사통제시스템, 기상 장비 등 발사를 위한 그리고 발사 후의 발사체 추적을 위한 장비가 건설 중이다. 본 글에서는 우주센터 기상장비 중에서 낙뢰현상을 감지할 수 있고 낙뢰의 이동방향을 추적할 수 있는 종합낙뢰감지시스템에 대하여 낙뢰의 관측방법과 국내외에서 낙뢰를 감지하여 실제 기상청이나 Launch Site에서 사용하고 있는 실례를 소개하고 우주센터에 설치 중인 종합낙뢰감지시스템의 성능과 앞으로의 활용가능성에 대하여 알아보기로 하겠다.

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Description of Range Control System in Space Center

  • Yun, Sek-Young;Choi,Yong-Tae;Lee, Hyo-Keun
    • 제어로봇시스템학회:학술대회논문집
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    • 2002.10a
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    • pp.53.2-53
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    • 2002
  • NARO Space Center is being developed as a national project for the Korea Space Development Program. Among the major missions of the Space Center, the Range Control System is the focal point for all command and control operation of the Space Center. The acquired data from the Tracking Stations and the on-site facilities is processed and distributed in the Control Center. Data processing or data fusion is needed for the exact tracking of the Launch Vehicle from several tracking systems. The first phase, which is the best telemetry source is selected among data streams that are received from each telemetry stations using some pre-defined criterion. Trajectory data and major telemetry parameters...

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Analysis on the Dynamic Characteristics of KOMPSAT-2 Shipping Container (다목적 실용위성2호 운송콘테이너의 동특성분석)

  • Kim, Hong-Bae;Woo, Sung-Hyun;Kim, Youngkey K.;Moon, Sang-Mu;Lee, Sang-Seol
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11a
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    • pp.356.1-356
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    • 2002
  • A satellite shipping container must afford the satellite a relatively benign thermal, vibration, and particle environment that is oblivious to the extreme temperatures, sand, dust, vibrations, and shock that can accompany the transportation. Korea Aerospace Research Institute has developed a new shipping container system that will be used to transport KOMPSAT-2(Korea Multi-Purpose SATellite) from Tae-jon to launch site. (omitted)

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A Study on the Dynamic Characteristics of S/C Shipping Container Isolation System (다목적 실용위성2호의 운송 콘테이너 개발)

  • 우성현;김홍배;문상무;김영기
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.11b
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    • pp.933-939
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    • 2001
  • A Satellite shipping container must afford the satellite a relatively benign thermal, vibration, and particle environment that is oblivious to the extreme temperatures, sand, dust, vibrations and shocks that can accompany the transportation. In this study, we have designed a vibration isolation system of a spacecraft container that will be used to transport a satellite called KOMPSAT (KOrea Multi-Purpose SATellite) -2 from KARI (Korea Aerospace Research Institute) Taejon to its launch site. To identify the dynamic characteristics of the system, a 1/3-scaled mockup of the container was developed. A large electro-magnetic shaker (Max. 240 KN) was used to excite the mockup, and vibration signals from 20 points were collected for modal tests. Numerical simulations through CATIA 3D Modeling were performed to identify the behavior of isolation springs. The results showed that a simplified model predicts the behavior in a reasonable accuracy. Moreover, the model guides us how to design a full-scaled satellite-shipping container.

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Automation of M.E.P Design Using Large Language Models (대형 언어 모델을 활용한 설비설계의 자동화)

  • Park, Kyung Kyu;Lee, Seung-Been;Seo, Min Jo;Kim, Si Uk;Choi, Won Jun;Kim, Chee Kyung
    • Proceedings of the Korean Institute of Building Construction Conference
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    • 2023.11a
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    • pp.237-238
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    • 2023
  • Urbanization and the increase in building scale have amplified the complexity of M.E.P design. Traditional design methods face limitations when considering intricate pathways and variables, leading to an emergent need for research in automated design. Initial algorithmic approaches encountered challenges in addressing complex architectural structures and the diversity of M.E.P types. However, with the launch of OpenAI's ChatGPT-3.5 beta version in 2022, new opportunities in the automated design sector were unlocked. ChatGPT, based on the Large Language Model (LLM), has the capability to deeply comprehend the logical structures and meanings within training data. This study analyzed the potential application and latent value of LLMs in M.E.P design. Ultimately, the implementation of LLM in M.E.P design will make genuine automated design feasible, which is anticipated to drive advancements across designs in the construction sector.

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First Light of the MIRIS, a Compact Wide-field Space IR Telescope

  • Han, Wonyong;Lee, Dae-Hee;Jeong, Woong-Seob;Park, Youngsik;Moon, Bongkon;Park, Sung-Joon;Pyo, Jeonghyun;Kim, Il-Joong;Park, Won-Kee;Lee, Duk-Hang;Seon, Kwang-Il;Nam, Uk-Won;Cha, Sang-Mok;Park, Kwijong;Park, Jang-Hyun;Yuk, In-Soo;Ree, Chang Hee;Jin, Ho;Yang, Sun Choel;Park, Hong-Young;Shin, Ku-Whan;Suh, Jeong-Ki;Rhee, Seung-Wu;Park, Jong-Oh;Lee, Hyung Mok;Matsumoto, Toshio
    • The Bulletin of The Korean Astronomical Society
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    • v.39 no.1
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    • pp.49.2-49.2
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    • 2014
  • The MIRIS (Multi-purpose InfraRed Imaging System) is a compact IR space Telescope, which has been developed by KASI since 2008 as the main payload of Korean STSAT-3. It was launched successfully by a Dnepr Rocket at Yasny Launch site, Russia in November 2013. After the launch, the STSAT-3 successfully settled down at Sun synchronous orbit with altitude of ~ 600km. Communications were regularly made between the ground station and the MIRIS with other secondary payload. We made a series of tests of the MIRIS during the verification period and found that all functions including the passive cooling are working as expected. The MIRIS has a wide-field of view $3.67{\times}3.67$ degrees and wavelength coverage from 0.9 to 2.0 micro-meter with the angular resolution of 51.6 arcsec. The main science missions of the MIRIS are (1) mapping of the Galactic plane with Paschen-alpha line (1.88 micro-meter) for the study of warm interstellar medium and (2) the measurement of large angular fluctuations of cosmic near infrared background radiation with I (1.05 micro meter) and H (1.6 micro meter) bands to identify their origin. We present the results of MIRIS initial operation in this paper.

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Legal Aspects of Insurance Regarding Space Activities and the Situation in China: an Analysis Based on the New Development of Space Commercialization (空間活動保險法律問題及中國狀況:基於空間商業化最新發展的分析)

  • Nie, Mingyan
    • The Korean Journal of Air & Space Law and Policy
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    • v.32 no.1
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    • pp.385-417
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    • 2017
  • Insurances of space activities are divided into satellite insurance, astronaut insurance and third party liability insurance. Against the background of the rapid development of space commercialization, especially the increasing participation of private entities in space affairs, the present international and domestic mechanisms of space insurance are challenged. As a space-faring state which is in the process of developing space businesses, the regulations of space insurance in China are deserved to be discussed. Satellites insurance is at present well-developed, the "pre-launch", "launch" and "in-orbit" phases of satellites are all possible to be insured by related companies. China created the CAIA in 1997 to provide insurance for Chinese satellites. However, with more private entities start to involve in space as well as satellite industry, the regime established under the framework of CAIA is necessary to be modified, and the mechanism relating to space insurance brokers should be promoted. The astronauts are recognized as the envoy of humankind, and relevant international regulations are made to provide assistance to them in emergency circumstances. From the domestic perspective, astronauts will be fully insured. China creates a particular type of insurance for astronauts. However, once space tourism becomes a business, the insurance of the tourist will be demanded to be created. In order to promote China's space tourism, it is recommended to take the "Astronaut Group Insurance" as an optional model to space tourists, if the tourists are customers of a governmental-owned space company. Once private involvement of providing orbital/suborbital tourism service becomes a reality, new rules are required. Getting a third party liability insurance is deemed as an indispensable precondition for an applicant to get a launch permission. Domestic space laws will include provisions for the third party liability insurance. China's "Interim Measures" of 2002 realizes the importance of third party liability insurance and requires the permit holder to get it before entering the launching site. This regulation is different from the practices of other states. Concerning that China is the sponsor of APSCO, for the purpose of promoting commercial space cooperation, a harmonized approach to domestic law is recommended to be found.

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