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Development of Advanced CMC Materials for Dual-bell Rocket Nozzles

Breede, Fabian and Frieß, Martin (2009) Development of Advanced CMC Materials for Dual-bell Rocket Nozzles. Project Report. DLR, Institut für Bauweisen- und Konstruktionsforschung.

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The main goal of sub-project D7 is the development of advanced ceramic matrix composites (CMCs) for a dual-bell application. These CMCs are characterized by continuous carbon filaments which are embedded in a silicon carbide matrix (SiC). The process route used for the manufacture of the so called C/C-SiC material is the Liquid Silicon Infiltration (LSI), also called Melt Infiltration (MI). The CMC material is favorable to replace conventional high-density engine alloys due to their outstanding high temperature properties. In a liquid-fueled rocket engine the material must withstand extreme conditions, e.g. high gas temperatures and high mechanical loads. In a first step the specifications and requirements of a CMC nozzle material have been defined and also the thermal and mechanical loads of a typical launcher system engine (e.g.Vulcain 2-Ariane 5) were described prior to the further development of C/C-SiC. A central part of the development is the integration of the filament winding process into the LSI route and the characterization of specimens in terms of thermo-mechanical properties by variation of fibre orientation. The analysis of permeability to hot gases and a study on oxidation behavior is planned in the upcoming year. The manufacturing process and the concept of characterizing the CMC material are presented and discussed.

Item URL in elib:https://elib.dlr.de/62882/
Document Type:Monograph (Project Report)
Title:Development of Advanced CMC Materials for Dual-bell Rocket Nozzles
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Breede, Fabianfabian.breede (at) dlr.deUNSPECIFIED
Frieß, Martinmartin.friess (at) dlr.deUNSPECIFIED
Journal or Publication Title:Sonderforschungsbereich Transregio 40 - Annual Reports
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
EditorsEmailEditor's ORCID iD
Lehrstuhl für Aerodynamik, TU MünchenUNSPECIFIEDUNSPECIFIED
Keywords:CMC, rocket nozzle, dual-bell, filament winding
Institution:DLR, Institut für Bauweisen- und Konstruktionsforschung
Department:Keramische Verbundstrukturen
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - HT-Werkstoffe und Bauweisen (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Ceramic Composite Structures
Deposited By: Friess, Dr.rer.nat. Martin
Deposited On:27 Jan 2010 09:43
Last Modified:31 Jul 2019 19:27

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