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  • Hot testing of laser welded channel wall nozzles on Vulcain 2 Engine and subscale stage combustion demo

    Paper number

    IAC-11,C4,3,7,x12052

    Author

    Mrs. Lise Brox, Volvo Aero Corporation, Sweden

    Coauthor

    Mr. Klas Lindblad, Volvo Aero Corporation, Sweden

    Coauthor

    Mr. Magnus Wir, Volvo Aero Corporation, Sweden

    Coauthor

    Mr. Sébastien Aknouche, Volvo Aero Corporation, Sweden

    Coauthor

    Mr. Ulf Palmnäs, Volvo Aero Corporation, Sweden

    Year

    2011

    Abstract
    Volvo Aero has for over ten years continuously developed and improved its patented
    manufacturing method for actively cooled nozzle extensions, i.e. the laser welded
    channel wall technology. Recently two different types of nozzles have been successfully
    tested in rigs operated by DLR in Lampholdshausen, Germany:
    
    \begin{itemize}\item The full scale Vulcain 2+ Nozzle Extension Demonstrator has now been
    successfully tested in two full scale hot firing tests on a Vulcain 2 engine in
    Lampholdshausen, Germany.\end{itemize}
    
    \begin{itemize}\item The SCENE subscale nozzle (Staged Combustion Engine Nozzle Extension)
    has been hot gas tested at the DLR test rig at in Lampoldshausen, during the
    summer of 2010.\end{itemize}
    
    The paper aims to give a good review the test results from the two test campaigns and an outline of the continued work ongoing at Volvo Aero in order to further mature both the sandwich nozzle technology.
    
    The Volvo Aero ambition has been to mature the sandwich cooled wall technology to TRL 6 in order to be ready for the next possible upgrade of the ARIANE 5 as well as other commercial launch vehicles. This goal is now achieved as the sandwich technology has reached TRL 6 by performing flawlessly in the two tests run, also making it eligible for other engine applications.
    
    The Vulcain 2+ NE Demonstrator project was performed under the auspices of SNSB, CNES, DLR and ESA, and performed in cooperation with Volvo Aero's industrial partners EADS Astrium and Snecma.
    Abstract document

    IAC-11,C4,3,7,x12052.brief.pdf

    Manuscript document

    IAC-11,C4,3,7,x12052.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.