Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
2010; American Institute of Aeronautics and Astronautics; Volume: 47; Issue: 5 Linguagem: Inglês
10.2514/1.42949
ISSN1533-6794
Autores Tópico(s)Diamond and Carbon-based Materials Research
ResumoCovers 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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