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首页|期刊导航|新型炭材料(中英文)|双脉冲固体火箭发动机中四向双基体炭/炭复合材料的非连续烧蚀行为

双脉冲固体火箭发动机中四向双基体炭/炭复合材料的非连续烧蚀行为

魏连锋 王润宁 张佳平 李克智 崔红

新型炭材料(中英文)2026,Vol.41Issue(3):707-720,14.
新型炭材料(中英文)2026,Vol.41Issue(3):707-720,14.DOI:10.1016/S1872-5805(26)61069-4

双脉冲固体火箭发动机中四向双基体炭/炭复合材料的非连续烧蚀行为

Discontinuous ablation behavior of four-directional dual-matrix C/C composites under dual-pulse solid rocket motors

魏连锋 1王润宁 2张佳平 2李克智 2崔红1

作者信息

  • 1. 西北工业大学 热结构复合材料科学技术实验室,陕西省纤维增强轻质复合材料重点实验室,陕西 西安,710072||西安航天复合材料研究所,陕西 西安,710025
  • 2. 西北工业大学 热结构复合材料科学技术实验室,陕西省纤维增强轻质复合材料重点实验室,陕西 西安,710072
  • 折叠

摘要

Abstract

Four-directional dual-matrix C/C composites were fabricated from PAN-based carbon fibers using a combined approach of soft-hard hybrid weaving pre-form molding,chemical vapor infiltration(CVI)of pyro-lytic carbon(PyC),high pressure impregnation and car-bonization of pitch-derived carbon.The ablation resist-ance of the composites was evaluated by testing in a dual-pulse solid rocket motor,and their ablation behavi-or was investigated.The carbon rods formed by twisting and carbonizing fiber bundles,exhibited a hexagonal cross-section,surrounded by a dense PyC"wall"structure formed during the CVI process.The linear ablation rates of the com-posites after pulse I and pulse Ⅱ were 0.068 mm/s and 0.113 mm/s,respectively.A cellular-like PyC layer and nanowire struc-tures were deposited on the surface of the throat convergent section during the post-combustion cooling phase,while cracks and delamination occurred on and within the divergent section.The ablation of C/C composites under these conditions was a com-plex multi-mechanism process,including ultra-high temperatures,high-speed gas scouring,oxygen-containing thermochemical ablation,and thermal shock.This work elucidates the ablation behaviors of C/C composites under dual-pulse conditions and provides technical guidance and a theoretical basis for designing and fabricating C/C composites for extreme ablation environ-ments.

关键词

C/C复合材料/烧蚀/双脉冲固体火箭发动机/微观结构演变/四向双基体

Key words

C/C composites/Ablation/Dual-pulse solid rocket motor/Microstructure evolution/Four-directional dual-matrix

分类

通用工业技术

引用本文复制引用

魏连锋,王润宁,张佳平,李克智,崔红..双脉冲固体火箭发动机中四向双基体炭/炭复合材料的非连续烧蚀行为[J].新型炭材料(中英文),2026,41(3):707-720,14.

基金项目

This work was supported by the National Natur-al Science Foundation of China(52272044,52125203),the fund of the Shaanxi Laboratory of Ad-vanced Materials(2024ZY-JCYJ-04-05)and the In-novation Foundation for Doctor Dissertation of North-western Polytechnical University(CX2025054). 国家自然科学基金(52272044、52125203) (52272044,52125203)

陕西省先进材料重点实验室开放基金(2024ZY-JCYJ-04-05)和西北工业大学博士论文创新基金(CX2025054). (2024ZY-JCYJ-04-05)

新型炭材料(中英文)

1007-8827

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