• 한국초전도ㆍ저온공학회논문지
• /
• 제17권4호
• /
• pp.43-46
• /
• 2015

The heavy ion accelerator that will be built in Daejeon utilizes four types of superconducting cavities. Cryomodules holding the superconducting cavities in them supply thermal insulation for cavities operating in 4.3 K or 2.1 K. A Prototype of cryomodule which holds two HWR (Half Wave Resonator) cavities was fabricated and tested. Since the operating temperature of the HWR is 2.1 K, the superfluid helium was generated with warm vacuum pumping system. The cyromodule was successfully cooled down below lambda point temperature of helium and any detectable leak was not observed during the test. The static thermal load at 4.2 K was measured. The result and the experience for the cool-down below lambda point of helium are reported in this paper.

• 한국항공우주학회지
• /
• 제45권8호
• /
• pp.678-685
• /
• 2017

지구관측위성에 탑재되는 자료처리/저장장치 방열판은 장비의 주기적인 고발열, 배치, 장착성 등 설계 특성으로 인해 쉴드가 장착된 홈 형태를 갖는다. 홈 형태 방열판의 영향성과 쉴드 방열판의 열성능을 확인하기 위해, 평판 방열판을 기준으로 홈 형태의 방열판과 쉴드 방열판을 비교하여 열진공 시험을 실시하였다. 시험결과를 바탕으로 view factor에 의한 열교환과 방열판의 온도를 이론해석적으로 분석하여 열 설계 성능비교의 타당성을 입증하였다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
• /
• 한국우주과학회 2010년도 한국우주과학회보 제19권1호
• /
• pp.37.4-37.4
• /
• 2010

KASI is developing the MIRIS (Multi-purpose IR Imaging System), as the main payload of Science and Technology Satellite-3 (STSAT-3). The Engineering Qualification Model (EQM) of the MIRIS has been recently fabricated, and Flight Model (FM) is now in final development stage. The system performance tests have been made mainly with EQM, and partly with FM in the laboratory, including opto-mechanics test, vibration test, thermal-vacuum test and passive cooling test down to 200K, using a thermal controlled vacuum chamber. Most of the system performance test results of the MIRIS are satisfied with the required specifications and its results were reflected in development of the FM with several revisions of the system design. In this paper, we present detailed system performance test procedures of the MIRIS and its results.

• 한국항공우주학회지
• /
• 제34권6호
• /
• pp.42-50
• /
• 2006

본 논문에서는 위성의 전장보드 열해석을 위한 최적의 열모델링 방법을 제안하였다. 플레이트 모델링 방법을 통한 보드 모델링에 고전력 소산 소자의 외부 및 내부 구조를 직접 모델링하는 방법을 새롭게 제안하였다. 이러한 모델링 방법을 다른 모델링과 비교 분석하여 효율성을 검토하였고 열진공 시험을 통해 검증하였다. 제시한 소자 모델링 방법으로 HAUSAT-2의 발열이 큰 통신보드의 열해석을 수행한 결과, 노드 네트워크 모델링 방법과 플레이트 모델링 방법의 단점을 모두 보완할 수 있었다. 또한, 소자 모델링 방법은 열적인 문제에 따른 소자 수준의 해결방안을 모색 후, 그에 따른 열해석을 수행하여 효과를 예측할 수 있으므로 열제어계 설계에도 효율적이다.

• Current Optics and Photonics
• /
• 제6권1호
• /
• pp.69-78
• /
• 2022

A high-resolution camera is a precise optical system. Its vibrations during transportation and launch, together with changes in temperature and gravity field in orbit, lead to different degrees of defocus of the camera. Thermal refocusing is one of the solutions to the problems related to in-orbit defocusing, but there are few relevant thermal refocusing mathematical models for systematic analysis and research. Therefore, to further research thermal refocusing systems by using the development of a high-resolution micro-nano satellite (CX6-02) super-resolution camera as an example, we established a thermal refocusing mathematical model based on the thermal elasticity theory on the basis of the secondary mirror position. The detailed design of the thermal refocusing system was carried out under the guidance of the mathematical model. Through optical-mechanical-thermal integration analysis and Zernike polynomial calculation, we found that the data error obtained was about 1%, and deformation in the secondary mirror surface conformed to the optical index, indicating the accuracy and reliability of the thermal refocusing mathematical model. In the final ground test, the thermal vacuum experimental verification data and in-orbit imaging results showed that the thermal refocusing system is consistent with the experimental data, and the performance is stable, which provides theoretical and technical support for the future development of a thermal refocusing space camera.

• 한국항공우주학회지
• /
• 제43권7호
• /
• pp.635-640
• /
• 2015

본 논문에서는 형상기억합금 구동기를 이용한 소형위성용 비폭발식 분리장치를 소개한다. 앞선 연구결과를 바탕으로 분리장치의 부품의 교체를 통하여 제안된 분리장치의 신뢰성을 향상시킴으로써 고사전하중(preload) 하에서도 구동이 가능하도록 하였다. 또한 충격 실험을 통하여 비폭발식분리장치의 장점인 저충격 발생을 확인하였고, 발사환경 및 우주 환경실험을 통하여 안정적으로 작동하는 것을 검증하였다. 결론적으로 본 연구에서는 충격실험, 진동실험 및 열진공실험 후 고사전하중에서 저충격을 발생시키며 안정적으로 작동 가능한 비폭발식 분리장치를 개발하였다.

• 한국진공학회:학술대회논문집
• /
• 한국진공학회 2012년도 제43회 하계 정기 학술대회 초록집
• /
• pp.229-229
• /
• 2012

Adhesion of Copper film on the aluminum oxide layer formed by anodizing an aluminum plate was enhanced by applying ion beam mixing method. Forming an conductive metal layer on the insulating oxide surface without using adhesive epoxy bonds provide metal-PCB(Printed Circuit Board) better thermal conductivities, which are crucial for high power electric device working condition. IBM (Ion beam mixing) process consists of 3 steps; a preliminary deposition of an film, ion beam bombardment, and additional deposition of film with a proper thickness for the application. For the deposition of the films, e-beam evaporation method was used and 70 KeV N-ions were applied for the ion beam bombardment in this work. Adhesions of the interfaces measured by the adhesive tape test and the pull-off test showed an enhancement with the aid of IBM and the adhesion of the ion-beam-mixed films were commercially acceptable. The mixing feature of the atoms near the interface was studied by scanning electron microscopy, Auger electron spectroscopy, and X-ray photoelectron spectroscopy.

• 한국윤활학회:학술대회논문집
• /
• 한국윤활학회 1997년도 제26회 추계학술대회
• /
• pp.66-75
• /
• 1997

This study was undertaken to investigate tribology characteristics of the alumina ceramics($Al_2O_3$) of the various purity for the variation of ambient condition such as air and vacuum. The wear test was carried out under different experimental condition using the wear test device, which was designed for this study, and in which the annular surface of wear testing specimens as well as mate specimen made of STB2 steel, were subjected to sliding speed, applied load and the sliding distance. The results obtained were as follows. As the ambient pressure decreases, the friction coefficient increases because the protective layer made of absorption due to decrease of the amount of ambient gas can not be formed. As the friction coefficient paticularly for 85% alumina lower than 95% and 99.7% in the alumina purity increases by an influence of heat accumulation caused by small elastic modulus and thermal conductivity. The friction surface of ceramics can be protected in the air by the influence of the oxides transfered from STB2. However, in the vacuum, the protective layer made of the absorption substance can not be formed due to the decrease of ambient gas.

• 한국항공우주학회지
• /
• 제43권1호
• /
• pp.72-78
• /
• 2015

오늘날 위성은 통신, 기상, 해양탐사, 광학, 레이다등 민수분야에서 군사분야까지 폭넓게 적용되어 그 유용성이 점점 더 증가되고 있다. 또한, 부품기술의 발달로 위성 전장품의 기능도 더욱 능동적인 형태로 진화되고 있다. 위성선진국에서는 통신위성의 중계기 효율을 증가시키고, 간섭신호를 제거하여 가입자 서비스 품질을 유지하기 위해서 디지털중계기를 탑재하고 있다. 디지털중계기는 다양한 기능구현을 위해 신호처리용 부품들을 다수 사용한다. 따라서, 기존의 수동형 중계기에 비해 많은 전력을 소모하여 더 높은 발열 상태를 유지한다. 본 논문에서는 우주인증모델(EQM)급으로 자체 제작된 디지털중계기 열진공 시험결과의 성능을 분석한다. 열진공시험과정중 디지털중계기의 기능검증을 위해 디지털 이득조정 시험결과를 제시한다. 또한, 열진공 시험결과를 근거로 주요부품의 부하경감(Derating)을 분석하여 디지털중계기 설계의 적절성을 논의한다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2004년도 추계학술대회
• /
• pp.545-550
• /
• 2004

KSTAR cryostat is a 8.8 m diameter vacuum vessel that provides the necessary thermal barrier between the ambient temperature test cell and the supercritical helium cooled superconducting magnet providing the base pressure of 1 ${\times}$ $10^{-3}Pa$. The cryostat is a single walled vessel consisting of central cylindrical section and two end closures, a flat base structure with external reinforcements and a dome-shaped lid structure. The base structure has 8 equally spaced support legs anchored on the concrete base. The cryostat vessel design was executed to satisfy the performance and operation requirements. The major loads considered in the structural analysis were vacuum pressure, dead weight, electromagnetic load driven by plasma disruption, and seismic load. Based on the fabrication and inspection procedures for the vessel, cryostat vessel was fabricated and inspected. It was confirmed that the inspection results were acceptable.