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Volumn 24, Issue 1, 2007, Pages 40-44

Ablation performance of C/C composites with different preforms

Author keywords

3D fine woven pierced felt structure; Ablation performance; Carbon carbon composites; Unidirectional carbon fiber needled bulk felt structure

Indexed keywords

ABLATION; EROSION; MECHANICAL PROPERTIES; SCANNING ELECTRON MICROSCOPY; SURFACE MORPHOLOGY; SURFACE ROUGHNESS; THERMAL CONDUCTIVITY;

EID: 34147201716     PISSN: 10003851     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (8)

References (12)
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  • 2
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    • Analysis of ablation of C/C composites
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  • 3
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    • Research and development of C/C composites for nozzles
    • Su Junming. Research and development of C/C composites for nozzles[J]. Carbon Science and Technology, 2001, 1(1): 6-11.
    • (2001) Carbon Science and Technology , vol.1 , Issue.1 , pp. 6-11
    • Su, J.1
  • 4
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    • Effects of nozzle contour in convergent section and throat on mass flow rate
    • Chen Linquan, Li Yanfang, Hou Xiao, et al. Effects of nozzle contour in convergent section and throat on mass flow rate[J]. Journal of Solid Rocket Technology, 2002, 25(1): 10-19.
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  • 5
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    • Investigation on ablation behavior of CFRC composites prepared at different pressure
    • Lee Young-Jae, Joo Hyeok Jong. Investigation on ablation behavior of CFRC composites prepared at different pressure[J]. Composites Part A, 2004, 35(11): 1285-1290.
    • (2004) Composites Part A , vol.35 , Issue.11 , pp. 1285-1290
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  • 6
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    • Zien T F. Thermal effects of particles on hypersonic ablation, AIAA-2001-2833[R]. Anaheim: AIAA, 2001.
    • (2001)
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  • 7
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    • Ablation analysis of the shuttle orbiter oxidation protected reinforced carbon-carbon, AIAA-94-2084
    • Colorado Springs: AIAA
    • Williams S D, Curry D M, Chao D C. Ablation analysis of the shuttle orbiter oxidation protected reinforced carbon-carbon, AIAA-94-2084[R]. Colorado Springs: AIAA, 1994.
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    • Williams, S.D.1    Curry, D.M.2    Chao, D.C.3
  • 8
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    • Hybrid rocket motor nozzle material predictions and results, AIAA-92-3591
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    • Bunker Robert C, Prince Andrew. Hybrid rocket motor nozzle material predictions and results, AIAA-92-3591[R]. Nashville: AIAA, 1992.
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  • 9
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    • Study on factors affecting ablative performance of C/C composites
    • Liu Jianjun, Su Junming, Chen Changle. Study on factors affecting ablative performance of C/C composites[J]. Carbon, 2003(2): 15-19.
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  • 10
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    • Microstructural interpretation of the effect of various matrices on the ablation performances of carbon fiber-reinforced composites
    • Cho Bong-Hwan, Byung Il-Yoon. Microstructural interpretation of the effect of various matrices on the ablation performances of carbon fiber-reinforced composites[J]. Composites Science and Technology, 2001, 61(2): 271-280.
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  • 11
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    • Influence of carbon-matrix structure on antiablative performances of C/C composites
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  • 12
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    • On improving anti-ablation property of multi-matrix C/C to withstand 3700 K
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.