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  • session 2

    Title

    Propulsion System (2)

    Description

    This session is dedicated to all aspects of Solid and Hybrid Propulsion.

    Date

    2018-10-02

    Time

    09:45

    Room

    ZARM 5

    IPC members
    • Co-Chair: Mr. Stéphane Henry, ArianeGroup, France;

    • Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;

    • Rapporteur: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    KEYNOTE: Recent developments in solid propulsion

    30

    confirmed

    Mr. Jean-Francois Guery

    ArianeGroup

    France

    2

    10:15

    Flight Results of Solid Propulsion System for Epsilon Launch Vehicle from the Third Flight

    15

    confirmed

    Dr. Koki Kitagawa

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    3

    10:30

    Research on thermochemical reaction mechanism and model of EPDM insulator under slag deposition condition

    15

    confirmed

    Dr. Yiwen Guan

    Northwestern Polytechnical University,NPU

    China

    4

    10:45

    Assessment of the Flight Experiments of a Multifunction Hybrid Sounding Rocket

    15

    confirmed

    Dr. Yen-Sen Chen

    American Institute of Aeronautics and Astronautics (AIAA)

    Taiwan, China

    5

    11:00

    Technology Development for a Potential Hybrid Mars Ascent Vehicle

    15

    confirmed

    Dr. Ashley Karp

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    6

    11:15

    Effect of Pressure Loss Devices on the Performance of Hybrid Rocket Systems

    15

    confirmed

    Prof.Dr. Arif Karabeyoglu

    Koc University

    United States

    7

    11:30

    A Study on Throttling, Anti-O/F Shift Operation and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method

    15

    confirmed

    Prof. Shigeru Aso

    Kyushu University

    Japan

    8

    11:45

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

    15

    confirmed

    Mr. Georg Poppe

    German Aerospace Center (DLR)

    Germany

    9

    12:00

    The preliminary study of severity level of structural discontinuities in paraffin grain of hybrid propellant rocket

    15

    confirmed

    Dr. Artem Andrianov

    University of Brasilia

    Brazil

    10

    12:15

    Experimental Investigation of the Feed System Instabilities in Hybrid Rocket Motors

    15

    confirmed

    Prof. Artur Bertoldi

    University of Brasilia

    Brazil

    11

    12:30

    Validation Against Experimental Data of Numerical Prediction of Characteristics of Combustion Instability in Hybrid Rocket Motors

    15

    confirmed

    Mr. Goutham Karthikeyan

    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

    Japan