Development of X-43A mach 10 leading edges

International Astronautical Federation - 56th International Astronautical Congress 2005

Volumn 8, Issue , 2005, Pages 5290-5298

  Ohlhorst, C W ^a   Glass, D E ^a   Bruce, W E ^a   Lindell, M C ^a   Vaughn, W L ^a   Smith, R W ^a   Dirling Jr , R B ^b   Hogenson, P A ^c   Nichols, J M ^d   Risner, N W ^d   Thompson, D R ^d   Kowbel, W ^e   Sullivan, B J ^f   Koenig, J R ^g   Cuneo, J C ^h  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b SCIENCE APPLICATIONS INTERNATIONAL CORPORATION   (United States)

^c BOEING COMPANY   (United States)

^d NORTHROP GRUMMAN CORPORATION   (United States)

^e MER CORPORATION   (United States)

^f Materials Research and Design Inc   (United States)

^g Materials Research Department

^h SOUTHERN RESEARCH INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL VAPOR DEPOSITION; IRIDIUM; MACH NUMBER; THERMAL CONDUCTIVITY; THERMAL EFFECTS;

CHEMICAL VAPORS; LEADING EDGES; THREE LAYER COATINGS;

SILICON CARBIDE;

EID: 34250844422     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.iac-05-d2.5.06     Document Type: Conference Paper

References (3)

1. th AIAA/CIRA International Space Planes and Hypersonics Systems and Technologies Conference, May 16-20, 2005.
2. Craig W. Ohlhorst, et al., "Thermal Conductivity Database of Various Structural Carbon-Carbon Composites," NASA TM 4787, November 1997.
3. Smith, Russell W.; Sikora, Joseph G.; and Lindell, Michael C.: Test and Analysis of a Hyper-X Carbon-Carbon Leading Edge Chine. NASA/TM -2005-213765, May 2005.