Application of Tyranno™ fiber/Si-Ti-C-O matrix composite to the thermal protection system of the Japanese HOPE-X space vehicle

Ceramic Engineering and Science Proceedings

Volumn 22, Issue 3, 2001, Pages 23-30

  Ogasawara, Toshio ^a   Ishikawa, Takashi ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

CREEP TESTING; ENTHALPY; FIBER REINFORCED MATERIALS; HEAT SHIELDING; OXIDATION; PLANNING; SEALANTS; SPACE APPLICATIONS; SURFACE TREATMENT; TENSILE STRENGTH;

CREEP STRENGTH; HIGH ENTHALPY CONVECTIVE ENVIRONMENT; POLYTITANOCARBOSILANE; THERMAL PROTECTION SYSTEM;

CERAMIC MATRIX COMPOSITES;

EID: 0035789853     PISSN: 01966219     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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