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  • session 5

    Title

    Propulsion Technology (2)

    type

    oral

    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    withdrawn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    withdrawn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    withdrawn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