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  • session 5

    Title

    Future Space Transportation Systems Technologies

    Description

    Discussion of technologies enabling new reusable or expendable launch vehicles and in-space transportation systems. Emphasis is on hardware development and verification before flight.

    Date

    2010-09-29

    Time

    15:15

    Room

    Chamber

    IPC members
    • Chairman: Prof. Yoshifumi Inatani, Japan Aerospace Exploration Agency (JAXA), Japan;

    • Chairman: Dr. Sylvain Guédron, Centre National d'Etudes Spatiales (CNES), France;

    • Rapporteur: Mr. William R. Claybaugh, II, Orbital Sciences Corporation, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    FLPP Technologies for a Future European Earth-to-Orbit Expendable Launcher

    15

    confirmed

    Mr. Guy Ramusat

    European Space Agency (ESA)

    France

    2

    Overview on technologies development applicable to cryogenic upper stages within ESA, Future Launchers Preparation Program (FLPP)

    15

    confirmed

    Mrs. Adriana Sirbi Paragina

    European Space Agency (ESA)

    France

    3

    Technological demonstrators Test Results

    15

    confirmed

    Dr. Sylvain Guédron

    ESA - APT

    France

    4

    high thrust engine demonstrations

    15

    confirmed

    Mr. Philippe Caisso

    Safran Aircraft Engines

    France

    5

    Catalytic bi-propellant ignition technology development

    15

    confirmed

    Mr. François Bouquet

    TNO Defence, Security & Safety

    The Netherlands

    6

    Conceptual study for the rocketplane experiment vehicle and the propulsion system

    15

    withdrawn

    Mr. Tetsuo Hiraiwa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    7

    ARES Project Technology Assessment - Approach and Tools -

    15

    confirmed

    Mr. Uwe Hueter

    Science Applications International Corporation (SAIC)

    United States

    8

    Technology Challenges for a Reusable First Stage

    15

    confirmed

    Dr. Jeffrey Zweber

    Air Force Research Laboratory (AFRL)

    United States

    9

    Neural Network Based Flush Air Data System (FADS) for Reusable Launch Vehicles

    15

    confirmed

    Mr. M. Jayakumar

    Indian Space Research Organization (ISRO)

    India

    10

    Continuous Twin Screw Technology for the Manufacture of Large Solid Propellant Grains of Next Generation Launcher

    15

    confirmed

    Mrs. Christine Marraud

    Safran SME

    France