Multiscale Approach to Ablation Modeling of Phenolic Impregnated Carbon Ablators
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.42681
Reference27 articles.
1. Post-Flight Evaluation of Stardust Sample Return Capsule Forebody Heatshield Material
2. Navier-Stokes Solutions with Finite Rate Ablation for Planetary Mission Earth Reentries
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