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  • session 6

    Title

    Future Space Transportation Systems Verification and In-Flight Experimentation

    Description

    Discussion of atmospheric and in-space flight testing and qualification of system, sub-system, and advanced technologies for future launch vehicles and in-space transportation systems. Emphasis is on higher TRL in-flight experimentation, demonstration, and qualification, including test plans and innovative technology prototype demonstrations involving or leading to flight as well as new and unique test platforms and capabilities.

    IPC members
    • Co-Chair: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;

    • Co-Chair: Dr. Christie Maddock, University of Strathclyde, United Kingdom;

    • Rapporteur: Mr. Tetsuo Hiraiwa, Japan Aerospace Exploration Agency (JAXA), Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    CALLISTO Demonstrator: Focus on system aspects

    15

    confirmed

    Dr. Sylvain Guédron

    Centre National d'Etudes Spatiales (CNES)

    France

    2

    Hypersonic Flight Experiment ReFEx: Status and Future Perspectives

    15

    confirmed

    Dr. Martin Sippel

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

    Germany

    3

    stort flight experiment for high speed technology demonstration

    15

    Prof.Dr. Ali Gülhan

    DLR (German Aerospace Center)

    Germany

    4

    system verifications for repeated operation by reusable vehicle experiment

    15

    Dr. Satoshi Nonaka

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    Reusability and Refurbishment approaches driving Space Rider platform engineering processes

    15

    Mr. ANGELO DENARO

    Thales Alenia Space Italia

    Italy

    6

    Space Cobot for in-orbit repair

    15

    confirmed

    Mrs. Marie-Christine Bernelin

    Dassault Aviation

    France

    7

    design modifications for performance enhancement of a suborbital rocket ilr-33 amber 2k

    15

    confirmed

    Mr. Michal Pakosz

    Łukasiewicz Research Network – Institute of Aviation

    Poland

    8

    Development of a low cost, low altitude test vehicle for high dynamic pressure parachute testing

    15

    confirmed

    Mr. Márton Géczi

    Delft Aerospace Rocket Engineering (DARE)

    The Netherlands

    9

    Low cost rocket guidance and aerodynamic control development platform

    15

    confirmed

    Mr. Dariusz Miedziński

    Warsaw University of Technology (WUT)

    Poland

    10

    Overview of the Twardowsky hybrid sounding rocket avionics design

    15

    withdrawn

    Mr. Karol Bresler

    Warsaw University of Technology (WUT)

    Poland

    11

    Sounding Rocket Research Infrastructure Developments

    15

    withdrawn

    Dr. Stefan Völk

    DLR (German Aerospace Center)

    Germany

    12

    Optimal preliminary design of hypersonic waverider using metaheuristics-based solutions.

    15

    confirmed

    Mr. Breno Silva

    Instituto de Estudos Avancados

    Brazil

    13

    Towards a Reusable First Stage Demonstrator: CALLISTO – Technical Progresses & Challenges

    15

    withdrawn

    Mr. Sven Krummen

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Institute of Space Systems

    Germany