항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제10권2호
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  • Pages.34-40
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  • 2016
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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차세대 소형위성 1호 충격시험 계측/분석 프로그램 개발

Development of Shock Test Measurement/Analysis Program for NEXTSat-1

  • 성태현 (순천대학교 우주항공공학전공) ;
  • 진재현 (순천대학교 우주항공공학전공) ;
  • 김상균 (한국과학기술원 인공위성연구센터)
  • Seong, Tae-hyeon (Division of Aerospace Engineering, Sunchon National University) ;
  • Jin, Jaehyun (Division of Aerospace Engineering, Sunchon National University) ;
  • Kim, Sang-kyun (Satellite Technology Research Center, Korea Advanced Institute of Science and Technology)
  • 투고 : 2016.02.03
  • 심사 : 2016.06.09
  • 발행 : 2016.06.30
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초록

A satellite is exposed to various impact environment until orbit entry. It is particularly undergoing the biggest impact by pyro shock, which is generated when the launch vehicle stages are separated or the satellite is separated from the launch vehicle. In this paper, due to the fact that the pyro shock is prerequisite for performing the test and verification on the ground, we developed an air-gun type shock tester for NEXTSat-1 shock test at the KAIST SaTReC along with the development of program introduced by LabVIEW software. The program operated in shock tester is consist of data measurement and analysis with the convenient implementation of user interface and its easy modification of the code.

키워드

참고문헌

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