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Featured researches published by Steffen Beyer.


Advances in Science and Technology | 2006

Advanced Composite Materials for Current and Future Propulsion and Industrial Applications

Steffen Beyer; Stephan Schmidt; Franz Maidl; Rolf Meistring; Marc Bouchez; Patrick Peres

Various technology programmes in Europe are concerned with preparing for future propulsion technologies to reduce the costs and increase the life time of components for liquid rocket engine components. One of the key roles to fulfil the future requirements and for realizing reusable and robust engine components is the use of modern and innovative materials. One of the key technologies which concern various engine manufacturers worldwide is the development of fibrereinforced ceramics – CMCs (Ceramic Matrix Composites). The advantages for the developers are obvious – the low specific weight, the high specific strength over a large temperature range, and their good damage tolerance compared to monolithic ceramics make this material class extremely interesting as a construction material. Different kind of composite materials are available and produced by EADS ST, the standard material SICARBON® (C/SiC made by Liquid Polymer Infiltration) and the new developed and qualified composite materials SICTEX® (C/SiC made by Liquid Silicon Infiltration) and CARBOTEX® (C/C made by Rapid Chemical Vapour Infiltration). The composites are based on textile techniques like weaving, braiding, stiching and sewing to produce multiaxial preforms, the SICTEX® material is densificated by the cost effective Liquid Silicon Infiltration (LSI). Over the past years, EADS Space Transportation (formerly DASA) has, together with various partners, worked intensively on developing components for airbreathing and liquid rocket engines. Since this, various prototype developments and hot firing-tests with nozzle extensions for upper and core stage engines and combustion chambers of satellite engines were conducted. MBDA France and EADS-ST have been working on the development of fuel-cooled composite structures like combustion chambers and nozzle extensions for future propulsion applications.


International Journal of Applied Ceramic Technology | 2005

Ceramic Matrix Composites: A Challenge in Space-Propulsion Technology Applications

Stephan Schmidt; Steffen Beyer; Hans Immich; Helmut Knabe; Rolf Meistring; Andreas Gessler


Ceramic Matrix Composites: Fiber Reinforced Ceramics and their Applications | 2008

The PIP‐Process: Precursor Properties and Applications

Günter Motz; Stephan Schmidt; Steffen Beyer


15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference | 2008

PTAH-SOCAR Fuel-Cooled Composite Materials Structure

Marc Bouchez; Steffen Beyer


Archive | 2003

Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture

Steffen Beyer; Helmut Knabe; Dieter Preclik


Archive | 2006

Interlaminar Properties of 2D and 3D C/C Composites Obtained via Rapid-CVI for Propulsion Systems

Ralf Knoche; Dietmar Koch; Kamen Tushtev; Jürgen Horvath; Georg Grathwohl; Stephan Schmidt; Steffen Beyer


Archive | 2004

Method for brazing ceramic surfaces

Steffen Beyer; Stephan Schmidt; Jan Hauptmann; Gunter Kirchhoff; Erich Prof.-Dr. Lugscheider


14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference | 2006

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

Marc Bouchez; Steffen Beyer


Archive | 2005

A process for producing moldings silicided

Steffen Beyer; Peter Greil; Rolf Meistring; Stephan Schmidt; Heino Sieber; Lars Weisenel


Archive | 2005

Brazing procedure for ceramic surfaces consists of preparing surfaces by creating holes of at least two different sizes in it

Steffen Beyer; Stephan Schmidt; Jan Hauptmann; Gunter Kirchhoff; Lugscheider, Erich, Prof.-Dr.

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Dietmar Koch

German Aerospace Center

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Heino Sieber

University of Erlangen-Nuremberg

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Peter Greil

University of Erlangen-Nuremberg

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