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http://dx.doi.org/10.5139/JKSAS.2012.40.7.555

A Study on the Damage of Satellite caused by Hypervelocity Impact with Orbital Debris  

Kang, Pil-Seong (한국과학기술원 기계공학과)
Im, Chan-Kyung (한국과학기술원 기계공학과)
Youn, Sung-Kie (한국과학기술원 기계공학과)
Lim, Jae-Hyuk (한국항공우주연구원)
Hwang, Do-Soon (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.40, no.7, 2012 , pp. 555-563 More about this Journal
Abstract
In earth orbit, a great number of orbital debris move around in extremely high velocity, and they become serious threats to satellites. In this study, smoothed particle hydrodynamics(SPH) is used to analyze the damage of a low earth orbit satellite due to the hypervelocity impact with orbital debris. The damage of honeycomb sandwich panel(HC/SP) used for walls of a satellite is analyzed with respect to impact velocities. For the additional analysis to examine the safety of interior components of the satellite, an attached electronic box and an offset electronic box are considered. As a result of the analysis considering the orbital debris having a probability of collision more than 2% at altitude of 685km, it is shown that the HC/SP can be perforated but only small craters are formed on both the attached electronic box and the offset electronic box.
Keywords
Smoothed Particle Hydrodynamics; Hypervelocity Impact; Orbital Debris; Satellite; Honeycomb Sandwich Panel;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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