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Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator

2010/09/01 by F. S. Milos, F. Milos, Y.-K. Chen · 5 citations
Mathematics · Engineering · Materials Science · #Gas Dynamics and Kinetic Theory #Rocket and propulsion systems research #Diamond and Carbon-based Materials Research

paper · doi:10.2514/1.42949

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

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