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  • D2
  • 4
  • session 4

    Title

    Future Space Transportation Systems

    type

    oral

    Description

    Discussion of future overall transportation system designs and operational concepts for both expendable and reusable systems for Earth-to-orbit transportation and exploration missions.

    IPC members
    • Co-Chair: Mr. José Gavira Izquierdo, European Space Agency (ESA), The Netherlands;

    • Co-Chair: Mr. Nicolas Bérend, ONERA - The French Aerospace Lab, France;

    • Rapporteur: Ms. Emmanuelle David, Ecole Polytechnique Fédérale de Lausanne (EPFL), Switzerland;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    High-Performance, Partially Reusable Launchers for Europe

    10

    confirmed

    Mr. Sven Stappert

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    4

    The design of the Space Rider Reentry Module GNC Subsystem up to CDR

    10

    confirmed

    Mr. Antonio Figueroa

    SENER

    Spain

    5

    Architecture and Ground operations concept for a Two Stage To Orbit using SABRE engines and launched from the CSG European Spaceport

    10

    confirmed

    Mr. Stephane Oriol

    CNES

    France

    6

    H3 Upgrade Concept with Enhanced Upper Compartment

    10

    confirmed

    Mr. Yorichika Mihara

    Mitsubishi Heavy Industries, Ltd.

    Japan

    8

    Multidisciplinary Optimisation of Future Reusable Space Vehicle

    10

    confirmed

    Mr. Sagar Satpathy

    Politecnico di Milano

    Italy

    9

    Preliminary Design Status of Unmanned Suborbital Spaceplane with LOX/Methane Engines by Tokyo University of Science’s Start-up with the Partnership of Industries: Part 2

    10

    confirmed

    Prof. Koichi Yonemoto

    Tokyo University of Science

    Japan

    10

    From the Earth to the Moon by gondola

    10

    confirmed

    Mr. Jean-Yves Prado

    PLATINEO

    France

    11

    Development of a tool for the analysis and optimisation of atmospheric re-entry trajectories

    10

    confirmed

    Mr. Luca Guerra

    Politecnico di Torino

    Italy

    12

    Method to Preset g-Load Profile of Launch Vehicles

    10

    confirmed

    Prof.Dr. Vitaly Yemets

    Oles Honchar Dnipropetrovsk National University

    Ukraine