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  • session 5

    Title

    Technologies for Future Space Transportation Systems

    Description

    Discussion of technologies enabling new reusable or expendable launch vehicles and in-space transportation systems. Emphasis is on early TRL hardware development and verification prior to flight, including ground testing and/or innovative technology prototype demonstrations not yet involving flight.

    IPC members
    • Co-Chair: Mr. Mathieu CHAIZE, ArianeGroup SAS, France;

    • Co-Chair: Prof. Lin Shen, China Academy of Launch Vehicle Technology (CALT), China;

    • Rapporteur: Mr. Andrea Esposito, Northrop Grumman Corporation, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A hybrid CMC/Metallic technology for the development of Space Rider reusable Body Flap Assembly Hot Structure

    Dr. Giuseppe Rufolo

    CIRA Italian Aerospace Research Centre

    Italy

    2

    Performance Improvement of VTOL Reusable Sounding Rocket with Air-breathing Engines towards Realizing Future Single-Stage-To-Orbit

    10

    confirmed

    Dr. Yusuke Maru

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    Advanced Modeling and Trajectory Optimization of the In-Air-Capturing Maneuver for Winged RLVs

    10

    confirmed

    Ms. Lâle Evrim Briese

    DLR, German Aerospace Center

    Germany

    4

    Aerial Recovery Technology of Launch Vehicle

    Dr. Xiaowei WANG

    China Academy of Launch Vehicle Technology (CALT)

    China

    5

    NAVIGA: A Modular Low-Cost Space Navigation Unit for Space Transportation

    10

    confirmed

    Mrs. Silvia Diaz

    SENER

    Spain

    6

    Development of a modular low-shock separation and jettison system

    10

    confirmed

    Dr. Alberto Sanchez Cebrian

    RUAG Space

    Switzerland

    7

    Thermal performance test of vacuum composite insulation material for Cryogenic Rocket Tank Based on cryocooler

    10

    confirmed

    Mr. shaohua zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    8

    An Improved Piston Pressurant System for Spacecraft Bipropellant Tanks

    withdrawn

    Mr. Noah Gula

    The Ohio State University

    United States

    9

    A reusable launch vehicle demonstrator for the future technology developments in Korea

    withdrawn

    Dr. Junseong Lee

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    10

    Model Predictive Control for reusable launcher guidance improvement

    10

    confirmed

    Mr. Jacopo Guadagnini

    Politecnico di Milano

    Italy

    11

    Complex numerical simulation of the launch system gas-dynamics

    10

    confirmed

    Mr. Serhii Furkalo

    Yuzhnoye State Design Office

    Ukraine

    12

    Flatness-based pseudospectral method for six-degree-of-freedom atmospheric entry trajectory planning

    Dr. Xu Liu

    Nanjing University of Aeronautics and Astronautics

    China

    13

    Preliminary Verification Strategy for Hybrid Navigation Systems (HNS) for Reusable Space Transportation Systems

    withdrawn

    Mr. René Schwarz

    German Aerospace Center (DLR)

    Germany

    14

    Real-time minimal modelling and parameter identification of liquid slosh dynamics

    withdrawn

    Dr. Hans Philipp Sueltrop

    New Zealand

    15

    Verification and Validation activities for the SPEAR mission

    10

    confirmed

    Ms. Esmée Menting

    Delft Aerospace Rocket Engineering (DARE)

    The Netherlands