Ablation behavior of C/C-SiC-ZrB2 composites in simulated solid rocket motor plumes

Yue Liu; Qiangang Fu; Beibei Wang; Yiwen Guan; Yang Liu

doi:10.1016/j.jallcom.2017.08.114

Ablation behavior of C/C-SiC-ZrB₂ composites in simulated solid rocket motor plumes

Yue Liu, Qiangang Fu, Beibei Wang, Yiwen Guan, Yang Liu

School of Materials Sience and Engineering

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

29 Scopus citations

Abstract

In order to improve the ablation resistance of carbon/carbon (C/C) composites, SiC-ZrB₂ was infiltrated into them by reactive melt infiltration (RMI). Their ablation behavior with a leading edge shape was investigated in the combustion environment of a simulated solid rocket motor (SRM). The results show that after introducing SiC-ZrB₂ ceramic phases into C/C composites, the linear and volume ablation rate of modified leading edge decreased by 26% and 45%, respectively. The high erosion rate of the composites leading edges was mainly attributed to the synergistic effect of thermochemical ablation and mechanical erosion in a high-velocity, high particle concentration two-phase flow of SRM plume environment.

Original language	English
Pages (from-to)	135-145
Number of pages	11
Journal	Journal of Alloys and Compounds
Volume	727
DOIs	https://doi.org/10.1016/j.jallcom.2017.08.114
State	Published - 15 Dec 2017

Keywords

Ceramic matrix composites
High temperature corrosion
SRM

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10.1016/j.jallcom.2017.08.114

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title = "Ablation behavior of C/C-SiC-ZrB2 composites in simulated solid rocket motor plumes",

abstract = "In order to improve the ablation resistance of carbon/carbon (C/C) composites, SiC-ZrB2 was infiltrated into them by reactive melt infiltration (RMI). Their ablation behavior with a leading edge shape was investigated in the combustion environment of a simulated solid rocket motor (SRM). The results show that after introducing SiC-ZrB2 ceramic phases into C/C composites, the linear and volume ablation rate of modified leading edge decreased by 26% and 45%, respectively. The high erosion rate of the composites leading edges was mainly attributed to the synergistic effect of thermochemical ablation and mechanical erosion in a high-velocity, high particle concentration two-phase flow of SRM plume environment.",

keywords = "Ceramic matrix composites, High temperature corrosion, SRM",

author = "Yue Liu and Qiangang Fu and Beibei Wang and Yiwen Guan and Yang Liu",

note = "Publisher Copyright: {\textcopyright} 2017",

year = "2017",

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doi = "10.1016/j.jallcom.2017.08.114",

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TY - JOUR

T1 - Ablation behavior of C/C-SiC-ZrB2 composites in simulated solid rocket motor plumes

AU - Liu, Yue

AU - Fu, Qiangang

AU - Wang, Beibei

AU - Guan, Yiwen

AU - Liu, Yang

PY - 2017/12/15

Y1 - 2017/12/15

N2 - In order to improve the ablation resistance of carbon/carbon (C/C) composites, SiC-ZrB2 was infiltrated into them by reactive melt infiltration (RMI). Their ablation behavior with a leading edge shape was investigated in the combustion environment of a simulated solid rocket motor (SRM). The results show that after introducing SiC-ZrB2 ceramic phases into C/C composites, the linear and volume ablation rate of modified leading edge decreased by 26% and 45%, respectively. The high erosion rate of the composites leading edges was mainly attributed to the synergistic effect of thermochemical ablation and mechanical erosion in a high-velocity, high particle concentration two-phase flow of SRM plume environment.

AB - In order to improve the ablation resistance of carbon/carbon (C/C) composites, SiC-ZrB2 was infiltrated into them by reactive melt infiltration (RMI). Their ablation behavior with a leading edge shape was investigated in the combustion environment of a simulated solid rocket motor (SRM). The results show that after introducing SiC-ZrB2 ceramic phases into C/C composites, the linear and volume ablation rate of modified leading edge decreased by 26% and 45%, respectively. The high erosion rate of the composites leading edges was mainly attributed to the synergistic effect of thermochemical ablation and mechanical erosion in a high-velocity, high particle concentration two-phase flow of SRM plume environment.

KW - Ceramic matrix composites

KW - High temperature corrosion

KW - SRM

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U2 - 10.1016/j.jallcom.2017.08.114

DO - 10.1016/j.jallcom.2017.08.114

M3 - 文章

AN - SCOPUS:85027579400

SN - 0925-8388

VL - 727

SP - 135

EP - 145

JO - Journal of Alloys and Compounds

JF - Journal of Alloys and Compounds

ER -

Ablation behavior of C/C-SiC-ZrB₂ composites in simulated solid rocket motor plumes

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Keywords

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