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Volumn 47, Issue 3, 2009, Pages 545-550

Ablation of pierced C/C composite nozzles in an oxygen/ethanol combustion gas generator

Author keywords

[No Author keywords available]

Indexed keywords

ATOMIZERS; CARBON FIBERS; COMBUSTION; FIRE PROTECTION; FIREPROOFING; FLAMMABILITY TESTING; GAS GENERATORS; GASES; METALLIC MATRIX COMPOSITES; NOZZLES; ROCKET ENGINES; SMOKE; THERMOCHEMISTRY;

EID: 58549118711     PISSN: 00086223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.carbon.2008.10.009     Document Type: Article
Times cited : (42)

References (17)
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  • 2
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  • 3
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    • Research on thermal gradient CVI process for preparing carbon/carbon composites
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    • Li, K.Z.1    Zhao, J.G.2    Li, A.J.3    Li, H.J.4
  • 7
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    • Ablation of solid-fuel booster nozzle materials
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  • 8
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  • 9
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  • 10
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    • The interaction of the efflux of solid propellant with nozzle materials
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    • Klager, K.1
  • 11
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    • (1985) Combust Sci Technol , vol.42 , Issue.3-4 , pp. 145-164
    • Kuo, K.K.1    Keswani, S.T.2
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    • Validation of an aerothermomechanical model for graphite nozzle recession and heat transfer processes
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  • 13
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.