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  • session 3

    Title

    Propulsion Technology

    Description

    This session includes all science and technology supporting all aspects of space propulsion.

    Date

    2010-09-29

    Time

    10:15

    Room

    Club A

    IPC members
    • Chairman: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;

    • Chairman: Dr. Carol J. Russo, National Aeronautics and Space Administration (NASA), United States;

    • Rapporteur: Mr. Alain Mercier, Snecma Propulsion Solide, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Experimental and numerical analyses of micro-scale jet nozzle flow

    15

    confirmed

    Mr. Seong-Up Ha

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    2

    CFD Multiphase Simulations of Cryogenic Tank Phenomena and their Verification by Tests

    15

    confirmed

    Mr. Juan Merino

    MT Aerospace AG

    Germany

    3

    SCENE Sub-Scale Nozzle Development and Testing

    15

    confirmed

    Mr. Klas Lindblad

    Volvo Aero Corporation

    Sweden

    4

    Low Cost Hydrazine Decomposition Catalyst (KCMC-7) Developed with Templating Method for Generation of Macropore for Facile Mass and Heat Transfer

    15

    confirmed

    Prof. Sung June Cho

    Chonnam National University

    Korea, Republic of

    5

    Demonstration of a full scale laser welded channel wall nozzle in hot test on the Vulcain 2 Engine

    15

    confirmed

    Mr. Roland Rydén

    Volvo Aero Corporation

    Sweden

    6

    catalytic decomposition of N2O using noble metals to develop monopropellant thruster

    15

    confirmed

    Mr. Assylkhan Kosdauletov

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    7

    Development of a Fuel Oxidiser Compatible Diaphragm

    15

    confirmed

    Mr. Derek Hancock

    MT Aerospace Satellite Products Ltd.

    United Kingdom

    8

    Evaluation and Characterization of Laser Ignition Conditions for GOX/GH2 Propellants

    15

    withdrawn

    Dr. Shinichi Moriya

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    Modeling and Experimental Verification of Auto-Ignition Processes for a Green Bi-Propellant Thruster

    15

    confirmed

    Mr. Markus Schiebl

    University of Applied Sciences Wiener Neustadt for Business and Engineering Ltd.

    Austria

    10

    The In-Space Propulsion (ISP-1) project

    15

    confirmed

    Mr. Michel Muszynski

    Safran Aircraft Engines

    France

    11

    Study on Decomposition of Green Propellant with Atmospheric Plasma for Plasma Chemical Thruster

    15

    confirmed

    Mr. Yuta Matsuura

    Tokyo Metropolitan University

    Japan

    12

    Vacuum testing of a micropropulsion system based on solid propellant cool gas generators

    15

    confirmed

    Mr. Alessandro Migliaccio

    Alten Sud Ouest

    France

    13

    Investigation of Hydrogen/Oxygen Small Thrust Rocket Engine using Gas Dynamic Resonance Technique

    15

    Mr. Nanjia Yu

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    14

    Numerical Simulation of the Ignition Process in a GOX/CH4 Vortex Thruster

    15

    confirmed

    Prof. Dechuan Sun

    China

    15

    development of a nitrous oxide monopropellant micro-thruster at buaa: 2009

    15

    confirmed

    Prof. Guobiao Cai

    Beijing University of Aeronautics and Astronautics (BUAA)

    China