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http://dx.doi.org/10.20910/JASE.2018.12.4.98

Structural Safety Evaluation of Electro-Optical Camera Controller Box of CAS500 Satellite under Launch Environments  

Lee, Myeong-Jae (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University)
Kim, Hyun-Soo (Hanwha Systems)
Lee, Duk-Kyu (Korea Aerospace Research Institute)
Oh, Hyun-Ung (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University)
Publication Information
Journal of Aerospace System Engineering / v.12, no.4, 2018 , pp. 98-105 More about this Journal
Abstract
The satellite is exposed to various launch environments such as random vibrations and shock. Accordingly, structural design of electronic equipment mounted on satellite must meet reliability requirements at the box level. In addition, it is essential to secure the reliability of the solder joint applied to electronic equipment. In this paper, we performed a modal and quasi-static analysis for the purpose of satisfaction of the design requirements of the CCB (Camera Controller Box) present on the 500 kg-class compact advanced satellite (CAS500). In addition, structural safety of electronic components was verified by the Steinberg's method and random equivalent static analysis.
Keywords
CCB(Camera Controller Box); Electronic Equipment; Fatigue Failure; Random Equivalent Static Analysis;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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