Validation of a Charring Ablator Material Response Code Against Oxyacetylene Torch Experiments on PICA Samples
Author:
Affiliation:
1. Massachusetts Institute of Technology
2. The University of Texas at Austin
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0862
Reference38 articles.
1. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
2. Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials
3. Chen, Y.K., and Milos, F., Three-Dimensional Ablation and Thermal Response Simulation System, https://doi.org/10. 2514/6.2005-5064, URL https://arc.aiaa.org/doi/abs/10.2514/6.2005-5064.
4. Detailed chemical equilibrium model for porous ablative materials
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