Conformal Phenolic Impregnated Carbon Ablator Arcjet Testing, Ablation, and Thermal Response
Author:
Affiliation:
1. Thermal Protection Materials Branch, NASA Ames Research Center, Moffett Field, California 94035-0001
2. Entry Systems Technology Division, ERC, Inc., Moffett Field, California 94035-0001
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.A33216
Reference9 articles.
1. Phenolic Impregnated Carbon Ablators (PICA) for Discovery class missions
2. Development of the Mars Science Laboratory Heatshield Thermal Protection System
3. An Overview of Technology Investments in the NASA Entry Systems Modeling Project
4. Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
5. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
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