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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

    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    withdrawn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    withdrawn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    withdrawn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