C/C-SiC Composites for Nozzle of Solid Propellant Ramjet

C/C-SiC Composites for Nozzle of Solid Propellant Ramjet

Carbon fiber reinforced carbon and silicon carbide matrix composites for nozzle inner of solid propellant ramjet were prepared by using the hybrid process of "chemical vapor infiltration + precursor impregnation pyrolysis (CVI+PIP)". The microstructure, flexural and anti-ablation propertie...

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Bibliographic Details
Main Authors: WANG Lingling, JI Alin, GAO Yaqi, CUI Hong, YAN Liansheng, PANG Fei
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2017-01-01
Series:Journal of Aeronautical Materials
Subjects:
C/C-SiC composites
solid propellant ramjet
nozzle inner
anti-ablative performance
motor hot firing
Online Access:http://jam.biam.ac.cn/CN/Y2017/V37/I1/80

Internet

http://jam.biam.ac.cn/CN/Y2017/V37/I1/80

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