A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures

Ryan, Shannon, Schaefer, F, Destefanis, R and Lambert, M 2008, A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures, Advances in Space Research, vol. 41, no. 7, pp. 1152-1166, doi: 10.1016/j.asr.2007.02.032.


Title A ballistic limit equation for hypervelocity impacts on composite honeycomb sandwich panel satellite structures
Author(s) Ryan, Shannon
Schaefer, F
Destefanis, R
Lambert, M
Journal name Advances in Space Research
Volume number 41
Issue number 7
Start page 1152
End page 1166
Total pages 15
Publisher ELSEVIER SCI LTD
Place of publication Vienna, AUSTRIA
Publication date 2008-01-01
ISSN 0273-1177
Keyword(s) Science & Technology
Technology
Physical Sciences
Engineering, Aerospace
Astronomy & Astrophysics
Geosciences, Multidisciplinary
Meteorology & Atmospheric Sciences
Engineering
Geology
space debris
hypervelocity impact
composites
CFRP
damage laws
ballistic limit equation
SHIELDS
Language eng
DOI 10.1016/j.asr.2007.02.032
Field of Research 0201 Astronomical and Space Sciences
0901 Aerospace Engineering
0913 Mechanical Engineering
HERDC Research category C1.1 Refereed article in a scholarly journal
Persistent URL http://hdl.handle.net/10536/DRO/DU:30149148

Document type: Journal Article
Collection: A2I2 (Applied Artificial Intelligence Institute)
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