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    Paper code

    IAC-18,C4,2,8,x42795

    Date

    2018-10-02

    Time

    09:45

    Order

    8

    Room

    ZARM 5

    Title

    Characterization of Regression Rate and Combustion Process in a High-Pressure 2D Hybrid Rocket Engine with Optical Access

    abstract

    View PDF

    Session

    2. Propulsion System (2)

    symposium

    C4. IAF SPACE PROPULSION SYMPOSIUM

    congress

    IAC-18

    Type of presentation

    oral

    Main author

    Mr. Georg Poppe, German Aerospace Center (DLR), Germany

    Co-authors

    Prof. Ognjan Božić, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    Mr. Stefan May, German Aerospace Center (DLR), Germany;

    Mrs. Nora M. Bierwagen, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    Mr. Rolfes Steffen, Germany;

    Mr. Patrick Koch, Germany;