Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-262
Reference32 articles.
1. 1Tran, H., Johnson, C, Rasky, D., Hui, F., Chen, Y.K., and Hsu, M. "Phenolic Impregnated Carbon Ablators (PICA) for Discovery ClassMissions,"AIAA Paper 96-1911,June 1996.
2. Stardust Sample Return Capsule Design Experience
3. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
4. Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials
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