• Composites Research
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• 제36권3호
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• pp.230-240
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• 2023

전개형 반사판 안테나는 단위 구조물 형태의 반사판이 접힌 상태로 수납되어 발사체에 탑재된 후, 운용궤도에 도달 및 전개되어 임무를 수행하는 위성체이다. 전개형 반사판 안테나는 수납 부피를 줄일 수 있어 발사체의 제한적 수납공간에 대형 우주 구조물을 탑재시킬 수 있으며, 경량소재를 적용할 경우 발사 및 운용 성능 향상에 용이한 장점이 있다. 본 논문에서는 전개형 반사판 안테나를 구성하는 주반사판에 대해 강성 및 강도 등의 구조적 분석을 통해 초기 개념설계를 수행하였다. 탄소섬유 복합재 및 허니콤 코어를 적용하여 경량 복합재 주반사판을 설계하였으며, 적층 패턴 및 형상을 설계 변수로 운용조건에 적합한 주반사판 설계안을 도출하였다. 이후 모드(Modal analysis), 준정적(Quasi-static), 열 구배(Thermal gradient) 및 동적(Dynamic) 거동에 대한 상세 구조해석을 수행하여 경량 복합재 반사판 안테나의 성능을 분석하였다

• 한국환경보건학회지
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• 제32권4호
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• pp.373-380
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• 2006

The photocatalytic reactor using immobilized $TiO_2$ on silicone sealant was studied bench scale using solar light as the source of radiation. The influences of parameters such as shape, polishing extent and size of reflector, distance between reactor and reflector, an angle of inclination between reactor system and ground, were studies using Rhodamine B (RhB) as a model compound. respectively. The decolorization of round type among the reflector shapes was higher than that of the polygon and W type. The polishing extent of the reflector did not show the decolorization largely. The optimum size of reflector and distance between reactor and reflector were 38 cm and 6 cm, respectively.

• 한국항해항만학회지
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• 제27권3호
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• pp.267-272
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• 2003

This paper describes design method of Passive-type Radar Reflector (PRR) which is to provide the requirement of newly revised 2000 SOLAS regulations on the Radar Reflector. The main target of this work is to find the optimum shape of a radar target having large Radar Cross Section (RCS). Through the RCS analysis based on the theoretical approach, two kinds of PRR models, RRR-F model for use in fisheries and PRR-S model for use in small sized ship, are designed and discussed their RCS performance. RCS measurement tests for the various sized samples are carried out in an anechoic chamber. As evaluation results it was clearly shown that the conventional sphere-type shows optimum shape in case of PRR-S, while the cylinder-type which consists of large sized corner clusters or zig-zag flat plats gives best performance in case of PRR-F.

• International Journal of Aerospace System Engineering
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• 제7권1호
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• pp.1-6
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• 2020

A deployment mechanism is designed to stow into a small volume efficiently. The panels are fabricated by carbon fiber reinforced plastics (CFRPs). The parameters for the deployment are determined by considering the number of panels, the folding/twisting angles, and the driving force for a deployment device. In addition, a surface accuracy of the manufactured reflector is measured through a photogrammetry methodology. The deployment behavior of CFRP reflector is observed by using the zero-gravity device which compensates the gravity effect during the deployment. The zero-gravity device is constructed wire, motor, controller and loadcell. During the deployment of the reflector panel, the wire and motor compensate for its weight by the feedback process of the controller. Tests result show that a zero-gravity device compensates for the weight of the panel during the deployment of the CFRP reflector.

• 한국환경과학회지
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• 제16권3호
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• pp.255-260
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• 2007

The photocatalytic decolorization of Rhodamine B (RhB) was studied using packed-bed reactor and immobilized $TiO_2/UV$ System. The 20 W UV-A, UV-B and UV-C lamps were employed as the light source. The effect of shape and surface polishing extent of reflector, distance between the reactor and reflector, reactor material were investigated. The results showed that the order of the initial reaction constant with reflector shape was round > polygon > W > rhombus. The optimum distance between the reactor and reflector was 2 cm. The initial reaction constant of quartz reactor was 1.46 times higher than that of tile PVDF reactor.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 1996년도 춘계학술대회 논문집
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• pp.170-176
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• 1996

A Sintered carbide roller mold for reflectors which is used for cover of automobile lamp and beacon plate of highway has been developed. The geometry of sintered carbide roller mold has been determined from the analysis of reflector geometry. An acute angle diamond wheel and dressing system also has been designed and developed to manufacture the sintered carbide roller mold.

• Journal of the Optical Society of Korea
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• 제17권5호
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• pp.371-375
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• 2013

To improve the utilization efficiency of solar energy, a new solar optical concentrating system composed of a parabolic reflector with a square cross-section, a hyperbolic reflector with a square cross-section and two converging convex lenses has been designed. The proposed method can simultaneously focus and shape sun light into a square pattern on the solar panel. In addition, the total reflection property of photonic crystal within the range of the visible sunlight spectrum has been analyzed. Finally, the relationship between solar concentrating multiples and the diameter of the primary mirror has been discussed.

• 한국전자통신학회논문지
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• 제9권2호
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• pp.255-260
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• 2014

최근에 열화상 카메라는 수 변전 설비의 열화 상태를 진단하는데 많이 사용하고 있다. 그러나 자장이 높은 곳에서는 열화상 카메라의 전자부가 높은 자장으로 인하여 제대로 동작하지 못하는 문제점이 발생한다. 이를 해결하기 위해 일반적으로 반사경을 사용할 수 있으나 반사경의 휨 등에 의해 반사 성능이 떨어지는 문제점이 있다. 본 논문에서는 이러한 문제점을 극복하기 위하여 아크릴 판에 알루미늄을 코팅하여 설계한 후 이를 제작하여 측정의 오차를 줄이고 측정 효율을 높이는 방법을 제시한다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 춘계학술대회 논문집
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• pp.897-900
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• 2002

The collimation mirror will be used for thermal vacuum testing of spacecraft. The reflection mirror system to generate parallel beam inside the thermal vacuum chamber. A 600mm diameter aspheric Collimation mirror was fabricated by ultra-precision single point diamond turning (SPDT). Aluminum alloy for mirror substrates is known to be easily machining, but not polishable due to its ductility. Aspheric large collimation reflector without a conventional polishing process, the surface roughness of 10nmRa, and the from error of $\lambda/2 ~\lambda/4(\lambda$ =632.8 nm) for reference curved surface 600 mm has been required. The purpose of this research is to find the optimum machining conditions for reflector cutting of A16061-T651 and apply the SPDT technique to the manufacturing of ultra precision optical components of metal aspheric reflector.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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• pp.254-257
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• 2007

This paper presents an examination of the spatial integration method for extracting the RCS of a trihedral corner reflector from SAR images for SAR external calibration. An exact external radiometric calibration technique is required for extracting an exact calibration constant. Therefore, we examine the accuracy of the spatial integration method, which is commonly used for the SAR external radiometric calibration. At first, an SAR image for a trihedral corner reflector is simulated with a high-resolution SAR impulse response with a known theoretical RCS of the reflector, and a background clutter image for the high resolution SAR system is also generated. Then, a SAR image in a high resolution is generated for a trihedral comer reflector located on a background clutter by superposition of the two SAR images. The radar cross section of a trihedral corner reflector in the SAR image is retrieved by integrating the radar signals of the pixels adjacent to the reflector for various size of the integration area. By comparison of the measured RCS by the integration method and the theoretical RCS of the reflector, the effect of the size of the integration area on the extraction of the calibration constant is examined.