Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
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American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
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Phenolic Impregnated Carbon Ablators (PICA) as Thermal Protection Systems for Discovery Missions
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Solution strategy for thermal response of nonablating thermal protection systems at hypersonic speeds
American Institute of Aeronautics and Astronautics |