Simulation of Orbital Debris Impact on Porous Ceramic Tiles
Author:
Affiliation:
1. Department of Mechanical Engineering, 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.A32658
Reference47 articles.
1. A Review of Ablation Modeling for Thermal Protection Systems
2. A Review of Numerical and Experimental Characterization of Thermal Protection Materials Part II: Properties Characterization
3. “Orbiter Thermal Protection System,” NASA Rept. FS-2004-09-014-KSC, 2004.
4. Parametric weight comparison of current and proposed thermal protection system (TPS) concepts
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