Erosion in Solid-Propellant Rocket Motor Nozzles with Unsteady Nonuniform Inlet Conditions
Author:
Affiliation:
1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
2. Buckmaster Research, Urbana, Illinois 61801
3. Lawrence Livermore National Laboratory, Livermore, California 94550
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/10.2514/1.47158
Reference26 articles.
1. A semiquantitative prediction of the erosion of graphite nozzle inserts
2. Erosion of graphite in solid-propellant combustion gases and effects on heat-transfer
3. A Comprehensive Theoretical Model for Carbon-Carbon Composite Nozzle Recession
4. Effect of Chamber Pressure and Propellant Composition on Erosion Rate of Graphite Rocket Nozzle
5. Chemical Erosion of Carbon-Carbon/Graphite Nozzles in Solid-Propellant Rocket Motors
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