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  • session 5

    Title

    Propulsion Technology (2)

    Description

    This session includes all science and technologies supporting all aspects of space propulsion. An objective is to attract papers from students and young professionals with a more technical rather than programmatic or organisational focus.

    Date

    2015-10-15

    Time

    09:45

    Room

    Ballroom B (Crowne Plaza Hotel, -1 floor)

    IPC members
    • Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;

    • Co-Chair: Mr. Max Calabro, The Inner Arch, France;

    • Rapporteur: Ms. Davina Di Cara, European Space Agency (ESA), The Netherlands;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Reusable Rocket Engine and It’s Tribological Subjects

    15'

    withdrawn

    Dr. Makoto Yoshida

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    2

    Advanced Sensor Technologies for Cryogenic Liquid Propellant Flow Phenomena

    15'

    confirmed

    Mr. Martin Siegl

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    3

    investigation of structural dynamics of high thrust lox/kerosene stage combustion cycle engine

    15'

    confirmed

    Dr. Fu Ping

    Xi'an Aerospace Propulsion Institute

    China

    4

    structural dynamic analysis of the lox/kerosene rocket engine based on synthetic technology for substructure test model

    15'

    no-show

    Dr. Feiping Du

    Xi'an Aerospace Propulsion Institute

    China

    5

    System frequency characteristics analysis for a large-thrust LOX/kerosene staged combustion cycle engine

    15'

    no-show

    Dr. Du Dahua

    College of Aeronautics, Northwestern Polytechnical University

    China

    6

    experimental investigation on distribution characteristics of mass flux and mixture ratio for unlike impinging injector

    15'

    no-show

    Mr. Yong Wang

    China

    7

    Analysis of frequency response characteristics of pressure-coupled liquid propellant vaporization process

    15'

    withdrawn

    Dr. Ganesh Paramasivan

    Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

    India

    8

    Energetic Characteristics of Nanoporous Silicon Impregnated with Different Oxidizers

    15'

    withdrawn

    Mrs. Evgenia Golda Kishilev

    Technion – Israel Institute of Technology

    Israel

    9

    Application of Multidisciplinary Design Optimization Method in Liquid Rocket Engine Design

    15'

    no-show

    Dr. Fu Ping

    Xi'an Aerospace Propulsion Institute

    China