PRORA-USV SHS: Ultra high temperature ceramic materials for sharp hot structures

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2005, Pages 597-612

  Scatteia, L ^a,b   Riccio, A ^a,c   Rufolo, G ^a,d   De Filippis, F ^a,e   Del Vecchio, A ^a,e   Marino, G ^a,f  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b Advanced Materials and Technology Lab   (Italy)

^c Computational Mechanics Lab ^*  (Italy)

^d Aerothermodynamics Lab   (Italy)

^e Plasma Wind Tunnel Unit   (United States)

^f Space Programs Office ^*  (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC MATERIALS; DATABASE SYSTEMS; FLIGHT DYNAMICS; HIGH TEMPERATURE EFFECTS; PLASMAS; PROJECT MANAGEMENT;

AERODYNAMIC DESIGN; HIGH TEMPERATURE CERAMIC MATERIALS; LAUNCH VEHICLES; SHARP HOT STRUCTURES (SHS);

AEROSPACE ENGINEERING;

EID: 29044440889     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3266     Document Type: Conference Paper

References (10)

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8. Caristia, S., De Filippis, F., Del Vecchio, A., Graps, E., "SCIROCCO PWT Facility for High Temperature Material Assembly Testing,", in Proceedings of 54th International Astronautical Congress, Bremen, 2003.
9. De Filippis, F., Del Vecchio, A., Caristia, S., "SCIROCCO Plasma Wind Tunnel: Low Enthalpy by use of cold air transverse injection", in Proceeding of 4th European Workshop on Thermal Protection Systems for Space Vehicles, Palermo, 2002.
10. Del Vecchio, A., De Filippis, F., "SCIROCCO Plasma Wind Tunnel: low enthalpy by use of cold air transverse injection," in Proceedings of 12th AIAA International Space Planes and Hypersonic Systems and Technologies, Norfolk, 2003.