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Official PDF TranslationNew Carbon Materials

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

Authors: Wei Lianfeng; Wang Running; Zhang Jiaping; Li Kezhi; Cui Hong

DOI: 10.1016/S1872-5805(26)61069-4Status: Verified Translated Edition
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Key Findings in This Report

• • Linear ablation rates of 0.068 mm/s (pulse I) and 0.113 mm/s (pulse II) demonstrate a 66% increase in ablation rate under dual-pulse conditions, indicating cumulative damage that must be accounted for in thermal protection design. • • The formation of a cellular-like PyC layer and carbon nanowires in the convergent section, catalyzed by ferrocene derivatives, reveals a deposition mechanism that can mitigate ablation but requires controlled pyrolysis conditions. • • Debonding at matrix-fiber, carbon rod-PyC, and within the PDC matrix interfaces led to crack initiation and delamination in the divergent section, highlighting the need for improved interfacial bonding to prevent mechanical erosion. • • The ablation process is characterized as discontinuous, involving high-temperature/high-velocity gas erosion, thermochemical ablation by oxygen-containing species, and thermal shock, necessitating multi-mechanism modeling for accurate lifetime prediction.