차세대 소형위성 1호 충격시험 계측/분석 프로그램 개발Development of Shock Test Measurement/Analysis Program for NEXTSat-1

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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.
Publisher
항공우주시스템공학회
Issue Date
2016-12
Language
Korean
Keywords

Air-gun Type Shock Tester; Design pattern; LabVIEW; Pyro shock; Uesr Interface

Citation

항공우주시스템공학회지, v.10, no.2, pp.34 - 40

ISSN
1976-6300
DOI
10.20910/JASE.2016.10.2.34
URI
http://hdl.handle.net/10203/223122
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