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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

    2014-10-02

    Time

    09:45

    Room

    714B

    IPC members
    • Co-Chair: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

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

    • Rapporteur: Mr. Jacques Gigou, European Space Agency (ESA), France;

    • Rapporteur: Dr. George Schmidt, NASA Glenn Research Center, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Airbus Defence and Space LOx/Methane propulsion demonstrators

    15'

    confirmed

    Mr. Roland Blasi

    Airbus Defence and Space

    Germany

    2

    Liquefied Gas Thruster with Ring Mechanism for Nanosatellite Propulsion

    15'

    confirmed

    Mr. Surmit Bhui

    University of Petroleum and Energy Studies

    India

    3

    lox/lh2 rocket engine health management applications of vibration analysis technology

    15'

    withdrawn

    Dr. Hui Wang

    Beijing Aerospace Propulsion Institute

    China

    4

    Cryogenic PVT-x Measurements of Helium-Hydrogen Mixtures

    15'

    withdrawn

    Mr. Ian Richardson

    Washington State University

    United States

    5

    Quantitative Visualization Studies of Self-Pressurizing Propellant Tank Dynamics

    15'

    withdrawn

    Mr. Andrew Ow

    Stanford University

    United States

    6

    New Innovative Liquid Fueled Rocket motor Manufacturing Methods: Additive Manufacturing in High Stress Applications

    15'

    confirmed

    Mr. Marten Jurg

    RMIT University, Australia

    Australia

    7

    A Linear Stability Analysis of Unique Low Frequency Mode on Uni-directional Vortex Injection Hybrid Rocket Engines

    15'

    confirmed

    Mr. Kohei Ozawa

    The University of TOKYO, Graduate school

    Japan

    8

    simulation-based multidisciplinary design optimization of the oxidizer pump in the turbopump system

    15'

    confirmed

    Mr. Yong Liao

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    9

    LOTUS : Standardized ESPA Propulsion System

    15'

    no-show

    Mr. Chrishma Singh-Derewa

    National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory

    United States

    10

    Measurement and Data Analysis of the South Korea’s Naro-1 Rocket Noise

    15'

    withdrawn

    Mr. SE HWAN PARK

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    11

    PERFORMANCE EVALUATION OF LANTHANUM DOPED CATALYST SUPPORT FOR A 50 N HYDROGEN PEROXIDE THRUSTER

    15'

    confirmed

    Mr. Shinjae Kang

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of