Effect of intermediate carbon/epoxy bumper orientation in spacecraft structural shielding
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Abrar | - |
| dc.contributor.author | 박유림 | - |
| dc.contributor.author | 김천곤 | - |
| dc.date.accessioned | 2014-12-08T08:41:30Z | - |
| dc.date.available | 2014-12-08T08:41:30Z | - |
| dc.date.created | 2014-10-08 | - |
| dc.date.issued | 2014-05-30 | - |
| dc.identifier.citation | 2014년도 한국복합재료학회 춘계학술대회, v., no., pp. - | - |
| dc.identifier.uri | http://hdl.handle.net/10203/191749 | - |
| dc.language | KOR | - |
| dc.publisher | 한국복합재료학회 | - |
| dc.title | Effect of intermediate carbon/epoxy bumper orientation in spacecraft structural shielding | - |
| dc.type | Conference | - |
| dc.type.rims | CONF | - |
| dc.citation.publicationname | 2014년도 한국복합재료학회 춘계학술대회 | - |
| dc.identifier.conferencecountry | South Korea | - |
| dc.contributor.localauthor | Abrar | - |
| dc.contributor.localauthor | 박유림 | - |
| dc.contributor.localauthor | 김천곤 | - |
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