People | Locations | Statistics |
---|---|---|
Naji, M. |
| |
Motta, Antonella |
| |
Aletan, Dirar |
| |
Mohamed, Tarek |
| |
Ertürk, Emre |
| |
Taccardi, Nicola |
| |
Kononenko, Denys |
| |
Petrov, R. H. | Madrid |
|
Alshaaer, Mazen | Brussels |
|
Bih, L. |
| |
Casati, R. |
| |
Muller, Hermance |
| |
Kočí, Jan | Prague |
|
Šuljagić, Marija |
| |
Kalteremidou, Kalliopi-Artemi | Brussels |
|
Azam, Siraj |
| |
Ospanova, Alyiya |
| |
Blanpain, Bart |
| |
Ali, M. A. |
| |
Popa, V. |
| |
Rančić, M. |
| |
Ollier, Nadège |
| |
Azevedo, Nuno Monteiro |
| |
Landes, Michael |
| |
Rignanese, Gian-Marco |
|
Elsäßer, Henning
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (1/1 displayed)
Places of action
Organizations | Location | People |
---|
document
Development of CMC Combustion Chambers for Advanced Propellants in Space Propulsion
Abstract
In the DLR project "Future Fuels", combustion chamber structures made of lightweight and high temperature stableceramic matrix composites were in the focus of the development. In a first step, C/C-SiC tubes manufactured via theliquid silicon infiltration process and based on three different carbon fibre types and two different productionmethods for the CFRP preforms, were characterized. In biaxial pressure tests, all the different tubes could withstandthe required inner pressure of 60 bar. Highest fracture strength was obtained with wet filament wound tubes based onultra-high-modulus fibres, whereas tubes manufactured via prepreg wrapping using high tenacity fibre fabrics,offered a cost-effective alternative.