PTAH-SOCAR Fuel-Cooled Composite Materials Structure for Dual-Mode Ramjet and Liquid Rocket Engines - Status 2006

Author:

Bouchez Marc1,Beyer Steffen2

Affiliation:

1. MBDA France

2. EADS Space Transportation

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. F.Falempin,D.Scherrer,G.Laruelle,Ph.Rostand,G. Fratacci, J.L.Schultz, "French hypersonic propulsion program PREPHA -results, lessons & perspectives", AIAA-98-1565-Norfolk,November1998.

2. F. Falempin, "PREPHA Program - System studies synthesis",XIII ISABE- Chattanooga-1997.

3. M. Bouchez, " Dual-mode ramjet thermo-mechanical design and associated performance", AIAA-2001-1918, Kyoto, Japan,April2001

4. Scotti, Martin, Lucas, «Active cooling design for scramjet engines using optimisation methods", AIAA88-2265

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2. Study on the Ablation Behavior of 3D Needled C/SiC in the Rocket Combustion Environments;Ceramic Transactions Series;2014-06-06

3. PTAH-SOCAR Fuel-Cooled Composite Materials Structure;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28

4. Prediction and Analysis of Heat Transfer in Small Rocket Chambers;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

5. Evaluation of Metallic-tube-cooled C/C Composite Structure by Rocket Combustor;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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