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  • session 3

    Title

    Propulsion Technology

    type

    oral

    Description

    This session includes all science and technologies supporting all aspects of space propulsion. The emphasis in this session is posed in particular on components for propulsion.

    Date

    2011-10-05

    Time

    10:00

    Room

    TS-06

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

    • Chairman: Mr. James Free, National Aeronautics and Space Administration (NASA), United States;

    • Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A New Fabrication Route for Ceramic MEMS-based Micropropulsion System - Soft Molding Technique using Submicron Alumina particles and Preceramic Polymer

    20

    confirmed

    Mr. Kean How Cheah

    University of Nottingham Malaysia Campus

    Malaysia

    2

    A SILICON-BASED MEMS RESISTOJET FOR PROPELLING CUBESATS

    20

    confirmed

    Mr. Tittu Varghese Mathew

    Switzerland

    3

    Development of a nitrous oxide monopropellant micro-thruster at buaa: 2010

    20

    confirmed

    Prof. Guobiao Cai

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    4

    Safety Evaluation of Hydroxyl Ammonium Nitrate(HAN) Based Monopropellants for Thrusters

    15

    confirmed

    Mr. Nobuyuki Azuma

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    LASER IGNITION OF ROCKET PROPELLANTS

    15

    withdrawn

    Prof. Sergey Rebrov

    Keldysh Research Center

    Russian Federation

    6

    Paraffin-Based Hybrid Rocket Testing At The Butte AeroTec Facility

    15

    confirmed

    Mr. David Micheletti

    United States

    7

    Hot testing of laser welded channel wall nozzles on Vulcain 2 Engine and subscale stage combustion demo

    15

    confirmed

    Mr. Ulf Palmnäs

    GKN Aerospace Engine Systems

    Sweden

    8

    Analysis of Thruster Exhaust Plume Impingement on Flexible Membrane of Solar Sail “IKAROS”

    15

    confirmed

    Mr. Norizumi Motooka

    University of Tokyo

    Japan

    9

    Research on the Radial Turbine Used in the LOX/Hydrogen Rocket Engine

    15

    no-show

    Mr. ZhongXiang Liu

    Beijing Aerospace Propulsion Institute

    China

    10

    Experimental and analytical characterization of shear coaxial GO2/GCH4 injector combustion flowfield

    15

    confirmed

    Dr. Yushan Gao

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    11

    Effective Stability Analysis of Liquid Rocket Combustion Chambers: Experimental Investigation of Damped Admittances

    15

    confirmed

    Mr. Thomas Fiala

    Technische Universität München

    Germany

    12

    Methane based hybrid rocket motor. Oxidizer doping model

    15

    confirmed

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania