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  • session 1

    Title

    Propulsion System (1)

    Description

    This session is dedicated to all aspects of Liquid Rocket Engines.

    Date

    2018-10-01

    Time

    15:00

    Room

    ZARM 5

    IPC members
    • Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Mr. Patrick Danous, ArianeGroup, France;

    • Rapporteur: Mr. Ozan Kara, Space Generation Advisory Council (SGAC), Turkey;

    • Rapporteur: Mr. Akira Ogawara, Mitsubishi Heavy Industries, Ltd., Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    KEYNOTE: The European Way for Liquid Propulsion – Hydrogen / Methane Family Concept

    20

    confirmed

    Dr. Gerald Hagemann

    ArianeGroup

    Germany

    2

    15:20

    Prometheus: Precursor of new low-cost rocket Engine Family

    12

    confirmed

    Mr. Roland Blasi

    ArianeGroup

    Germany

    3

    15:32

    600-kN Reusable LOX/Methane Rocket Engine Research and Development

    12

    withdrawn

    Mr. Dayong Zheng

    Beijing Aerospace Propulsion Institute

    China

    4

    15:44

    Vinci Upper Stage Engine Development, Test, Qualification, and Industrialisation Status for Ariane 6

    12

    confirmed

    Mr. Dietrich Haeseler

    ArianeGroup

    Germany

    5

    15:56

    Result of Preliminary Design and Development Status of LE-9 Engine

    12

    confirmed

    Mr. Akihide Kurosu

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    16:08

    analysis and verification of the spaceil lunar lander propulsion system during development and breadboard testing

    12

    withdrawn

    Mr. Avichai Elimelech

    Israel Aerospace Industries Ltd.

    Israel

    7

    16:20

    progress in 30kn lox/methane expander cycle engine

    12

    confirmed

    Mr. Shengqing Cheng

    Beijing Aerospace Propulsion Institute

    China

    8

    16:32

    FLPP ETID: Hot-Fire Test Results of Future European Expander Technologies

    12

    confirmed

    Dr. Thomas Fuhrmann

    ArianeGroup

    Germany

    9

    16:44

    leading progress of chemical rocket engines in China

    12

    withdrawn

    Dr. Fashu Shi

    CALT,CASC

    China

    10

    16:56

    Modelling and Correlation of Cryogenic Orbital Stages with Focus on Propellant Tanks

    12

    confirmed

    Mr. Danail Nedyalkov-Höfkes

    ArianeGroup

    Germany

    11

    17:08

    the design and test of 1N thruster with HAN-based propellant

    12

    withdrawn

    Mr. chuan Liu

    Shanghai Insitute of Space Propulsion

    China

    12

    17:20

    Qualification approach for modifications of Liquid Propulsion Systems

    12

    confirmed

    Mr. DUSSOLLIER Gabriel

    ArianeGroup SAS

    France

    13

    17:32

    Current status of the LUMEN LOX/LNG rocket engine demonstrator

    12

    withdrawn

    Dr. Jan Deeken

    DLR (German Aerospace Center)

    Germany

    14

    17:44

    Damage Mitigating Analysis for Liquid Rocket Engine of Next Reusable Launch Vehicle

    12

    confirmed

    Mr. ren jiawan

    China

    15

    17:56

    Latest Progress of High Performance Liquid Apogee Engine for Satellites in SISP

    12

    confirmed

    Mr. Changguo Liu

    Shanghai Institute of Space Propulsion

    China

    16

    18:08

    Status of the evaluation of the Vinci rocket engine Oxygen chill-down with COMETE thermal-hydraulic software.

    12

    Mr. Charles-Hubert Bachelet

    ArianeGroup

    France