A comparison of ballistic limit with adaptive-mesh Eulerian hydrocode predictions of one- and two-plate aluminum shielding protection against millimeter-sized Fe

A comparison of ballistic limit with adaptive-mesh Eulerian hydrocode predictions of one- and two-plate aluminum shielding protection against millimeter-sized Fe–Ni space debris

Published:2008-12 Issue:12 Volume:35 Page:1602-1605
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Horner J.K.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference21 articles.

1. Liou J-C, et al. The new NASA orbital debris engineering model 2000 (ORDEM2000). NASA TP-2002-210780; May 2002.

2. Christiansen EL. Meteoroid/debris shielding. NASA TP-2003-210788; August 2003.

3. Encyclopedia of the solar system,2007

4. Elsevier. International Journal of Impact Engineering. http://www.elsevier.com/.

5. Finite volume methods for hyperbolic problems;Leveque,2002

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