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http://dx.doi.org/10.5139/JKSAS.2009.37.6.586

Spectrum and Equivalent Transient Vibration Analysis of Small Composite Satellite Structure  

Cho, Hee-Keun (KAIST 인공위성연구센터)
Seo, Jung-Ki (KAIST 인공위성연구센터)
Myung, Noh-Hoon (KAIST 인공위성연구센터)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.37, no.6, 2009 , pp. 586-594 More about this Journal
Abstract
This paper is the study on random, sinusoidal and shock vibration responses for the STSAT-3(science and technology satellite-3) proto-model which is the first small size all-composite satellite in Korea. The structure system of the STSAT-3 forms box type structure by joining several hybrid sandwich panels comprised of honeycomb core and carbon fiber reinforced laminated composite skins on both side. Mode shape, stress, displacement and acceleration responses are obtained on both the frequency domain and time domain by means of a commercial FEA software MSC/NASTRAN. From these analysis results, failure, safety factor and design validity are assessed. These results can be successfully applicable as reference data when a new satellite is developed as well as giving out an excellent criteria in satellite vibration treatment design.
Keywords
Satellite; Composite; Vibration; Sandwich;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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