Thermochemical Erosion Analysis for Chraphite/Carbon-Carbon Rocket Nozzles
Author:
Affiliation:
1. University of Rome “La Sapienza”, 00184 Rome, Italy
2. Second University of Naples, 81131 Caserta, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.47754
Reference24 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
4. Aerothermochemical analysis of carbon-carbon nozzle regression in solid-propellant rocket motors
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