한국생산제조학회지 (Journal of the Korean Society of Manufacturing Technology Engineers)

  • 제24권1호
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  • Pages.87-93
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  • 2015
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  • 2508-5093(pISSN)
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  • 2508-5107(eISSN)
한국생산제조학회 (The Korean Society of Manufacturing Technology Engineers)
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우주용 광학구조체의 진동응답 평가

Dynamic Response Assessment of Space Use Telescope

  • Cho, Hee Keun (Department of Mechanical Engineering Education, Andong National University)
  • 투고 : 2014.12.03
  • 심사 : 2015.01.08
  • 발행 : 2015.02.15
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초록

The dynamic responses of a telescope loaded on an STSAT-3 satellite were analyzed, and environmental tests were conducted to verify the reliability of the design. The space use telescope COMIS (compact imaging spectrometer) is a major payload of the STSAT-3 launched on November 21, 2013. Vibration responses such as the acceleration, displacement, and velocity with respect to random vibration and shock impulse inputs were obtained based on theoretical fundamentals in conjunction with finite element analysis. The main focus of this study was on developing technology for accurate and/or favorable modeling and analysis of the structure and fitting the results to that of experiments. Cutting-edge technology for manipulating the vibrations of a space use telescope is suggested.

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참고문헌

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피인용 문헌

  1. On-orbit Thermal Analysis of the Instrument for the Study of Space Storm vol.29, pp.1, 2020, https://doi.org/10.7735/ksmte.2020.29.1.35
  2. Structural and Thermal Analyses of Image Processing Units of Satellites vol.29, pp.1, 2015, https://doi.org/10.7735/ksmte.2020.29.1.42