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A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures
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2008
Journal Article
Titel
A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures
Author(s)
Ryan, S.
Schäfer, F.
Destefanis, R.
Lambert, M.
Zeitschrift
Advances in Space Research
DOI
10.1016/j.asr.2007.02.032
Language
English
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Fraunhofer-Institut für Kurzzeitdynamik Ernst-Mach-Institut EMI