Thermochemical Erosion Analysis of Carbon-Carbon Nozzles in Solid-Propellant Rocket Motors
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Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
1. The Interaction of the Efflux of Solid Propellants with Nozzle Materials
2. A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession
3. Validation of an Aerothermochemical Model for Graphite Nozzle Recession and Heat-Transfer Processes
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