Composite technologies development status for scramjet applications

12th AIAA International Space Planes and Hypersonic Systems and Technologies

Volumn , Issue , 2003, Pages

  Bouquet, C ^a   Fischer, R ^a   Larrieu, J M ^a   Uhrig, G ^a   Thebault, J ^a  

^a SNECMA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ADVANCED COMPOSITES; COMPOSITE TECHNOLOGY; DEVELOPMENT STATUS; FLIGHT CONDITIONS; SCRAMJET COMBUSTORS; SILICON CARBIDE COMPOSITES; STRUCTURAL DEVELOPMENT; TECHNOLOGICAL DEVELOPMENT;

CARBON SILICON CARBIDE COMPOSITES; COMBUSTION CHAMBERS; COMBUSTORS; COMPOSITE MATERIALS; DESIGN;

TECHNOLOGY;

EID: 84896788203     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Carbon-Carbon Extendible Nozzles, M. Lacoste, A. Lacombe, P. Joyez SEP & R.A.Ellis, JC Lee, FM. Payne Pratt&Whitney IAF-97-S.2.04 Turin Oct 97
2. Carbon-Carbon Nozzle Extension for the RL10B-2 rocket Engine, R.A. Ellis Pratt & Whitney, M. Lacoste SNECMA/SEP IAF-99-S.2.06 oct 99 AMSTERDAM
3. th Symposium of the energetics panel on airbreathing propulsion for missiles and projectiles. May 11-15, 1992
4. Towards an all composite scramjet combustor, G. Uhrig, JM. Larrieu Snecma Propulsion Solide AIAA 2002-3883 Indianapolis Jul 2002
5. Direct Fuel Cooled Composite Structure D. G. Medwick, J.Castro, Pratt&Whitney, D.R. Sobel UTRC, G. Boyet Onera J.P. Vidal Snecma Propulsion Solide AIAA SL-233/USA-54