Radius of Curvature Effects on Throat Thermochemical Erosion in Solid Rocket Motors
Author:
Affiliation:
1. Dipartimento di Ingegneria Meccanica e Aerospaziale, University of Rome “La Sapienza,” 00184 Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32944
Reference39 articles.
1. Internal Ballistics Modeling of High Performance SRMs with Coupled Nozzle Erosion Characterization
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5. A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession
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