The Energy absorption profile for Spacecraft first bumper made of Carbon-Epoxy composite under hypervelocity impacts in Low Earth Orbit environment

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Publisher
The Korean Society for Composite Materials
Issue Date
2011-11-17
Language
ENG
Citation

The 8th Korea-Japan Joint Symposium on Composite Materials

URI
http://hdl.handle.net/10203/191836
Appears in Collection
AE-Conference Papers(학술회의논문)
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