Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Glass, David E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AUTOMOBILE MANUFACTURE; CERAMIC MATRIX COMPOSITES; CONTROL SURFACES; EARTH ATMOSPHERE; HEAT SHIELDING; HYPERSONIC AERODYNAMICS; ORBITS; ROCKETS; SPACE SHUTTLES; THERMAL INSULATING MATERIALS;

ACCESS TO SPACE VEHICLES; AIR BREATHING VEHICLES; ENVIRONMENTAL DURABILITY; HYPERSONIC CRUISE VEHICLE; MANAGEMENT TECHNIQUES; SINGLE STAGE TO ORBITS; SPACE SHUTTLE ORBITER; THERMAL PROTECTION SYSTEM;

HYPERSONIC VEHICLES;

EID: 77958475723     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2682     Document Type: Conference Paper

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