Simulation of Foam-Impact Effects on the Space Shuttle Thermal Protection System
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.6759
Reference19 articles.
1. Impact Testing of Large Foam Projectiles
2. Foam-on-Tile Impact Modeling for the STS-107 Investigation
3. CTH: A three-dimensional shock wave physics code
4. Analyses of Foam Impact onto the Columbia Shuttle Wing Leading Edge Panels Using Pronto3d/SPH
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