• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1194-1197
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• 2005

Micro nozzle is employed as a dynamic passive valve in micro fluidic devices. Micro nozzle array is used in micro droplet generation in bio-medical applications and propulsion device for actuating satellite and aerospace ship in vacuum environments. Aperture angle and the channel length of the micro nozzle affect its retification efficiency, and thus it is needed to produce micro nozzle precisely. MEMS process has a limit on making a micro nozzle with high-aspect ratio. Reactive ion etching process can make high-aspect ratio structure, but it is difficult to make the complex shape. Focused ion beam deposition has advantage in machining of three-dimensional complex structures of sub-micron size. Moreover, it is possible to monitor machining process and to correct defected part at simultaneously. In this study, focused ion beam deposition was applied to micro nozzle production.

• 한국위성정보통신학회논문지
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• 제7권2호
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• pp.54-58
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• 2012

본 논문에서는 사용자가 존재할 때만 LED 조명을 활성화해서 통신 기능을 수행하고 사용자가 없을 때에는 자동으로 LED 조명을 비활성화 할 수 있는 종합 제어 시스템 기반 기술을 디자인하고 구현하였다. 이 시스템은 마이크로 콘트롤러를 이용한 사용자 감지기능을 수행하는 HW 모듈과 웹을 통한 종합 제어 시스템 SW 모듈로 구성된다. 마이크로 콘트롤러 보드는 ATMega2560를 이용하여 설계하고, 적외선과 초음파 센서를 이용하여 사용자 유무를 판단하였으며, 웹 기반의 모니터링 시스템은 스마트 디바이스를 통해서 제어할 수 있도록 구성하였다. 두 모듈의 연동 테스트를 통해서 본 시스템의 유효성을 검증하였다.

• 품질경영학회지
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• 제51권3호
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• pp.461-479
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• 2023

Purpose: It emphasizes the importance of cost analysis for weapons systems that require enormous develop- ment costs, analyzes the problems of cost analysis steps from a practical point of view, and presents the direction of business development in terms of cost analysis reliability, timeliness, and efficiency. Methods: It analyzes the R&D cost of Micro satellites with a complex cost structure and large scale according to engineering estimation procedures, derives major analysis step-by-step problems, and presents business development directions. Results: Problems with standards and assumptions, data collection, cost division structure, and cost estimation methods were derived through the micro satellite cost analysis process, and business development directions such as expanding common standards, standardizing basic data, standardizing cost division structures and cost items, and data asset were presented. Conclusion: In order to develop work in terms of cost analysis reliability, timeliness, and efficiency, it is important to prepare and standardize standards and rules for detailed tasks at each analysis stage, and through this, it is expected that high utilization value and systematic cost data will be assetized in the future.

• International Journal of Aeronautical and Space Sciences
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• 제12권3호
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• pp.283-287
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• 2011

Science and Technology Satellite-3 (STSAT-3) is a 150 kg class micro satellite based with the national space program. The STSAT-3 system consists of a space segment, ground segment, launch service segment, and various external interfaces including additional ground stations to support launch and early operation phases. The major ground segment is the ground station at the Satellite Technology Research Center, Korea Advanced Institute of Science and Technology site. The ground station provides the capability to monitor and control STSAT-3, conduct STSAT-3 mission planning, and receive, process, and distribute STSAT-3 payload data to satisfy the overall missions of STSAT-3. The ground station consists of the mission control element and the data receiving element. This ground station is designed with the concept of low cost and high efficiency. In this paper, the requirements and design of the ground station that has been developed are examined.

• 전산구조공학
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• 제22권6호
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• pp.25-36
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• 2009

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.1052-1054
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• 2003

RAZAKSAT is a second micro-satellite mission by Malaysian Satellite Program and is expected for launch in June 2004. Designed to orbit the earth at low-equatorial orbit, RAZAKSAT will meet Malaysia’s immediate needs to rapid data acquisition (real time and more repetitions) to address many operational issues of remote sensing applications, which require availability of current data sets. RAZAKSAT will be among the first remote sensing satellite to orbit the earth at low inclination along the equator, 9$^{\circ}$ with 685km altitude, hence, allows optimal geographical information and environment change within equatorial region be observed with a unique revisit characteristics. The satellite primary payload is MAC, a push-broom type camera with 2.5m of ground sampling distance (GSD) in panchromatic band and 5m of GSD in four multi-spectral bands. This paper describes on the variation of illumination anticipated from simulated RAZAKSAT image, examine its implication to its ground leaving radiances for major applications.

• Animal cells and systems
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• 제15권1호
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• pp.37-43
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• 2011

The Korean freshwater crayfish, Cambaroides similis, has recently suffered from range reduction and habitat degradation caused by environmental changes and water pollution. For the conservation and restoration of this species, it is necessary to understand the current population structures of Korean C. similis using estimation of their genetic variation. In this study, eight micro satellite loci were developed and characterized from 49 individuals collected from four locations: one population from Mt. Bukhan (BH) and three populations from Mt. Gwanak (GA) in Seoul, Korea. As a result, the number of alleles per locus ranged from 2 to 12. The observed heterozygosities and expected heterozygosities ranged from 0.000 to 0.833 and from 0.125 to 0.943, respectively, and the former values were significantly lower than the latter ones expected under the Hardy-Weinberg equilibrium. No significant linkage disequilibrium was revealed between any of the locus pairs after Bonferroni correction. From the pairwise Fst results over all samples, higher differentiation between GA-BH population pairs (mean 0.1789) was observed than between GA population pairs (mean 0.0454). This was also supported by Mantel's test showing that the genetic distances of these crayfish populations were significantly correlated with geographic distances. This result may show the regional differentiation caused by restricted gene flow between northern (BH) and southern (GA) populations within Seoul. These micro satellite markers have the potential for use in analyses of the genetic diversity and population structure of C. similis species, with implications for its conservation and management plans.

• 한국소음진동공학회논문집
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• 제25권1호
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• pp.24-32
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• 2015

Pulse tube-type spaceborne cryocooler is widely used to cool down the infrared sensor of observation satellites. However, such cryocooler also generates micro-vibration which is the one of main sources to seriously affect the image quality during its on-orbit operation. Therefore, to comply with the mission requirement of high resolution observation satellite, additional technical efforts have been required. In this study, we proposed a spaceborne cryocooler passive vibration isolator using SMA mesh washer, which guarantees the structural safety of both the micro-vibration disturbance source and itself under harsh launch vibration loads without an additional holding mechanism and the micro-vibration isolation performance on orbit environment. To verify the micro-vibration isolation performance of the proposed vibration isolator, we performed the micro-vibration isolation measurement test using the dedicated micro-vibration measurement device proposed in this study.

• 한국추진공학회지
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• 제11권6호
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• pp.42-49
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• 2007

본 연구에서는 마이크로 추진장치의 개발을 위한 기초연구로 마이크로 노즐의 유동 특성을 분석하였다. 냉가스 추진원리를 이용하였으며, 추진 장치의 노즐 목 직경이 1.0, 0.5, 0.25 mm 인 마이크로 노즐을 방전가공을 이용하여 제작하였다. 판스프링과 스트레인 게이지를 이용한 추력측정장치를 이용하여 추력을 측정하였으며, 대기압 환경과 진공환경에서 마이크로 노즐의 유동특성을 분석하였다. 추진제는 아르곤과 질소를 사용하였으며, 실험 결과를 CFD 결과와 비교하였다. 연구 결과 노즐의 소형화로 인해 점성과 배압에 의한 유동손실이 발생함을 확인할 수 있었다.

• 우주기술과 응용
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• 제1권1호
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• pp.33-40
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• 2021

본 논문에서는 총 무게 42 kg 이내의 요구사항을 토대로 차세대소형위성 2호 영상 레이다 시스템을 개발한 결과를 보고한다. 차세대소형위성 2호는 소형급 인공위성으로, 탑재체의 무게 비중이 전체 무게 대비 약 40% 정도를 차지하도록 설계하였다. 영상 레이다 시스템은 안테나, RF송수신기, 기저대역 신호처리기, 전력부 등으로 구성되며, 이 중에서 특히 무게 비중이 큰 부품은 영상 레이다의 핵심인 안테나이다. 안테나 설계시 이득, 효율 등을 고려한 다양한 선택이 가능하지만, 차세대소형위성 2호 사업에서 요구하는 무게, 전력 및 해상도 등을 반영하여 Micro-strip Patch Array 안테나를 채택하여 설계하였다. 차세대소형위성 2호의 임무 요구 조건에 부합하도록 안테나의 주파수는 9.65 GHz, 이득은 42.7 dBi 그리고 반사손실은 -15 dB로 규정하여 개발하였으며, 차량에 탑재한 현장시험을 통하여 요구 성능의 충족 여부를 검증하였다.