Ablation and thermal response property model validation for Phenolic Impregnated Carbon Ablator

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Milos, F S ^a   Chen, Y K ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ABLATORS; CHAR DEPTH; CREW MODULE; ELEMENTAL COMPOSITIONS; HEAT CAPACITIES; IMPREGNATED CARBONS; MODEL PREDICTION; MODEL VALIDATION; RESPONSE MODEL; SURFACE TEMPERATURES; TEST CONDITION; THERMAL DECOMPOSITIONS; THERMAL PROPERTIES; THERMAL RESPONSE; TRANSVERSELY ISOTROPIC;

ABLATION; AEROSPACE ENGINEERING; FORECASTING; HEAT FLUX; PHENOLS; PYROLYSIS; THERMOANALYSIS;

THERMAL CONDUCTIVITY;

EID: 78549242320     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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