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  • session 4

    Title

    Future Space Transportation Systems

    type

    oral

    Description

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

    Date

    2017-09-27

    Time

    14:45

    Room

    Hall O

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

    • Co-Chair: Mr. Charles E. Cockrell Jr., National Aeronautics and Space Administration (NASA), United States;

    • Rapporteur: Mrs. Philippa Davies, Reaction Engines Ltd., United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    HTV-X system integration plan

    18

    confirmed

    Mr. daisuke tsujita

    Mitsubishi Heavy Industries Ltd. - Nagoya Aerospace Systems

    Japan

    2

    Ariane Next : weighting options for the next generation of Ariane launchers.

    18

    confirmed

    Mr. Jerome VILA

    Centre National d'Etudes Spatiales (CNES)

    France

    3

    Evaluation of Future Ariane Reusable VTOL Booster Stages

    18

    confirmed

    Mr. Etienne Dumont

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

    Germany

    4

    Systematic Assessment of Reusable First-Stage Return Options

    18

    confirmed

    Dr. Martin Sippel

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

    Germany

    5

    DREAM CHASER FOR EUROPEAN UTILIZATION (DC4EU): ESA PILOT PHASE RESULTS

    18

    confirmed

    Dr. Marco Berg

    OHB System

    Germany

    6

    Development plan and demonstration of Japanese reusable launch vehicle

    18

    confirmed

    Mr. Kotaro Aoki

    Mitsubishi Heavy Industries Ltd. Japan

    Japan

    7

    design and ground test of an rbcc based two-stage-to-orbit reusable launch vehicle

    18

    confirmed

    Dr. Chunlin Gong

    Northwestern Polytechnical University,NPU

    China

    8

    A Conceptual Analysis and Comparison of a Two-Stage-To-Orbit Reusable Launch Vehicle Using Airbreathing Precooling Hypersonic Engines

    18

    no-show

    Dr. Jianxing Zhou

    Beijing Aerospace Technology Institute

    China

    9

    A feasibility study and conceptual proposal of a reusable multistage winged space transportation system with tandem orbiter-carrier connection by horizontal take-off and landing

    18

    confirmed

    Mr. Yang Tianyang

    Moscow Aviation Institute (National Research University, MAI)

    Russian Federation

    10

    Multidisciplinary Shape Optimization of Reusable Space Vehicle

    18

    withdrawn

    Mr. Sagar Satpathy

    Politecnico di Milano

    Italy

    11

    Preliminary Design for Modular SEP Tug Utilizing Dream Chaser Cargo Module

    18

    confirmed

    Mr. Jonathan Grimm

    The Ohio State University College of Engineering

    United States