Effect of honeycomb core under hypervelocity impact: numerical simulation and engineering model

Author:

Chen Hong,Francesconi Alessandro,Liu Sen,Lan Shengwei

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference9 articles.

1. R. Putzar, F. Schäfer, H. Stokes, F. Chant, M. Lambert, Vulnerability of spacecraft electronics boxes to hypervelocity impacts, Proceedings of the 56th IAC, 2005, Fukuoka Japan, 17–21 October 2005.

2. Vulnerability of spacecraft harnesses to hypervelocity impacts;Putzar;Int. J. Impact Eng.,2008

3. F. Schäfer, R. Putzar, M. Lambert, Vulnerability of satellite equipment to hypervelocity impacts, Proceedings of the 59th IAC, 2008, Glasgow, Scotland, 29 Septe mber–3 October 2008.

4. Y. H. Huo, Z. T. Tang, H. Y. Han. The hypervelocity impact experiment investigation and analysis on thermal control instrument in satellites, Proceedings of the 61th IAC, 2010, 27 September - 1 October 2010, Prague, Czech Republic 2010.

5. Hypervelocity Impact On Spacecraft Honeycomb Hydrocode Simulation And Damage Laws;Taylor;Int. J. Impact Eng.,2003

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