Ablation behavior of SiC fiber/carbon matrix composites under simulated atmospheric reentry conditions

Composites Part A: Applied Science and Manufacturing

Volumn 42, Issue 3, 2011, Pages 221-228

  Ogasawara, Toshio ^a   Aoki, Takuya ^a   Hassan, Mohamed Sayed Aly ^a   Mizokami, Yosuke ^b,c   Watanabe, Naoyuki ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO METROPOLITAN UNIVERSITY   (Japan)

^c IHI CORPORATION   (Japan)

Author keywords

A. Carbon carbon composites (CCCs); A. Ceramic matrix composites (CMCs); B. High temperature properties; D. Thermal analysis

Indexed keywords

A-CARBON; A-THERMAL; AIR PLASMAS; ATMOSPHERIC RE-ENTRY; MASS LOSS RATE; MATRIX COMPOSITE; PLASMA WIND TUNNELS; POLYMER IMPREGNATION AND PYROLYSIS; RE-ENTRY VEHICLES; SHORT DURATIONS; SIC FIBERS; SURFACE RECESSION; THERMAL ANALYSIS; ULTIMATE TENSILE STRENGTH; WOVEN FABRICS; Z-DIRECTIONS;

CARBON CARBON COMPOSITES; CARBON FIBERS; CARBON SILICON CARBIDE COMPOSITES; CERAMIC MATERIALS; CHEMICAL VAPOR INFILTRATION; CRACKING (CHEMICAL); MECHANICAL PROPERTIES; REENTRY; SILICON CARBIDE; TENSILE STRENGTH; THERMOANALYSIS; WIND TUNNELS;

ABLATION;

EID: 79151480348     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesa.2010.10.015     Document Type: Article

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