Towards an all composite SCRAMJET combustor

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Uhrig, G ^a   Larrieu, J M ^a  

^a SNECMA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

CYCLIC LIVES; FLIGHT CONDITIONS; PAPER DOCUMENTS; SCRAMJET COMBUSTORS; SCRAMJET TEST; SILICON CARBIDE COMPOSITES; THERMAL MARGINS; WEIGHT SAVING;

COMBUSTION CHAMBERS; COMPOSITE MATERIALS; PROPULSION;

COMBUSTORS;

EID: 84896692795     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

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. Application des matériaux thermostructuraux aux chambres de combustion pour statoréacteurs D. CRAPIZ SEP AGARD-79th Symposium of the energetics panel on airbreathing propulsion for missiles and projectiles. May 11-15, 1992.