UPDATED ABLATION AND THERMAL RESPONSE PROGRAM FOR SPACECRAFT HEATSHIELD ANALYSIS Frank S. Milos, Yih-Kanq Chen, and Thomas H. Squire

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Date: 2006-07-27 09:08:15 Heat transfer Heat conduction Thermal protection Atmospheric entry Spaceflight Pyrolysis R-value Space Shuttle thermal protection system Ablation Chemistry Chemical engineering Mechanical engineering		UPDATED ABLATION AND THERMAL RESPONSE PROGRAM FOR SPACECRAFT HEATSHIELD ANALYSIS Frank S. Milos, Yih-Kanq Chen, and Thomas H. Squire Add to Reading List Source URL: tfaws.nasa.gov Download Document from Source Website File Size: 4,04 MB Share Document on Facebook

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