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  • session 2

    Title

    Propulsion Systems II

    Description

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

    Date

    2009-10-13

    Time

    10:00

    Room

    Technical Session #15

    IPC members
    • Chairman: Mr. Jean-François Guery, Safran SME, France;

    • Chairman: Dr. I-Shih Chang, The Aerospace Corporation, United States;

    • Rapporteur: Dr. Gennaro Russo, Campania Aerospace District, DAC, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Combustion Instability of Solid Rocket Motor with Complicated Grain Shape

    20'

    Dr. Daning Hu

    China

    2

    Two minutes inside the A5 SRM : Effects of different source of pressure oscillations during operation

    20'

    Ms. BALLEREAU Séverine

    Safran SME

    France

    3

    controllable solid rocket motor throttleability and accurate continuous thrust adjustment

    20'

    Prof. Giuseppe Lombardo

    Università degli Studi di Palermo

    Italy

    4

    a test study of underwater ignition of solid rocket motor

    20'

    Mr. Youjun Jia

    Academy of Aerospace Propulsion Technology, China Aerospace Science and Technology Corporation (CASC)

    China

    5

    Development and Experimental Study on Kick Motor Igniter of KSLV-I

    20'

    Dr. Hyeonseok Koh

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    6

    ABOUT STABILITY OF ROCKET PROPULSION USING PASTE-LIKE PROPELLANT

    20'

    Mr. Konstantin Prisniakov

    M. S. Polyakov Institute of Geotechnical Mechanics, National Academy of Sciences of Ukraine

    Ukraine

    7

    hybrid rocket engine, theoretical model and experiment

    20'

    Prof. Teodor-Viorel Chelaru

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    8

    combustion characteristics of the end-burning hybrid rockets at laminar flow

    20'

    Dr. Tsuneyoshi Matsuoka

    Hokkaido University

    Japan

    9

    Computation and Experiment of Fuel Regression Rate in GOX-HTPB Hybrid Rocket Motors

    20'

    Dr. Hui Tian

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    10

    an experimental study on rocket propulsion by reaction of mg-based propellant and water

    20'

    Mr. Liya Huang

    China

    rocket propulsion using unitary paste-like propellant. designs for using in composition of planetary landing units and upper stages of launch vehicles

    Mr. Yulian Protsan

    The Laboratory of Advanced Jet Propulsion

    Ukraine