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  • session 2

    Title

    Propulsion System (2)

    type

    oral

    Description

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

    Date

    2017-09-26

    Time

    09:45

    Room

    Hall E3

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

    KEYNOTE: Boris Novozhilov: Life and Contribution to the Physics of Combustion

    30'

    confirmed

    Prof. Vasily Novozhilov

    University of Victoria

    2

    Development of Solid Propulsion System for Enhanced Epsilon Launch Vehicle and Epsilon’s Second Launch Results

    15

    confirmed

    Dr. Koki Kitagawa

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    3

    ariane 6 and vega c programs, the p120C nozzle

    15

    confirmed

    Mr. ERIC GAUTRONNEAU

    Airbus Safran Launchers

    France

    4

    Solid Rocket Motor Technology Development for the Torogoz Sounding Rocket Program

    15

    withdrawn

    Mr. Luis Salaverria

    EL Salvador Aerospace Institute (ESAI)

    El Salvador

    5

    Development of a Multi-function Hybrid Sounding Rocket

    15

    confirmed

    Dr. Yen-Sen Chen

    American Institute of Aeronautics and Astronautics (AIAA)

    Taiwan, China

    6

    Enhanced Solid Propellant Burn Rate Measurement Technique Using X-Ray Real-Time Radiography

    15

    withdrawn

    Mr. Ali Butt

    United States

    7

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

    15

    no-show

    Prof.Dr. arif karabeyoglu

    Koc University

    United States

    8

    Optical Analysis of Liquid Film Instabilities in Paraffin-based Hybrid Rocket Fuels

    15

    confirmed

    Ms. Anna Petrarolo

    German Aerospace Center (DLR)

    Germany

    10

    Throttling Capability and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method

    15

    confirmed

    Prof. Shigeru Aso

    Kyushu University

    Japan

    11

    numerical and experimental study of graphite nozzle erosion in hybrid rocket motor with star grain

    15

    confirmed

    Dr. Hui Tian

    Beihang University

    China

    12

    Combustion Performance of a Staged Hybrid Rocket with Boron addition

    15

    confirmed

    Mr. Dongeun Lee

    Konkuk University

    Korea, Republic of

    The Performance Analysis of the SARA Hybrid Rocket Motor

    withdrawn

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil