Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles

Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles

Ultra-high-temperature ceramic matrix composites (UHTCMCs) based on a ZrB2/SiC matrix have been investigated for the fabrication of reusable nozzles for propulsion. Three de Laval nozzle prototypes, obtained by sintering with either hot pressing (HP) or spark plasma sintering (SPS), were tested 2–3...

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Bibliographic Details
Main Authors: Diletta Sciti, Antonio Vinci, Luca Zoli, Pietro Galizia, Simone Failla, Stefano Mungiguerra, Giuseppe D. Di Martino, Anselmo Cecere, Raffaele Savino
Format: Article
Language:English
Published: Tsinghua University Press 2023-07-01
Series:Journal of Advanced Ceramics
Subjects:
ultra-high-temperature ceramics (uhtcs)
ceramic matrix composites (cmcs)
propulsion
oxidation resistance
nozzle prototypes
Online Access:https://www.sciopen.com/article/10.26599/JAC.2023.9220759

Internet

https://www.sciopen.com/article/10.26599/JAC.2023.9220759

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