Ultra-High-Temperature Ceramic Matrix Composites in Hybrid Rocket Propulsion Environment
Author:
Affiliation:
1. University of Naples "Federico II"
2. National Research Council (CNR)
3. TECNALIA
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4694
Reference30 articles.
1. Chemical Erosion of Carbon-Carbon/Graphite Nozzles in Solid-Propellant Rocket Motors
2. Investigation of Graphite Nozzle-Throat-Erosion in a Laboratory-Scale Hybrid Rocket Using GOX and HDPE
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