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  • session 1

    Title

    Liquid Propulsion (1)

    type

    oral

    Description

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

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

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

    • Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Research and Development of 500 ton- Thrust-Class LOX/kerosene Rocket Engine

    30

    confirmed

    Prof.Dr. Hui Chen

    Xi'an Aerospace Propulsion Institute

    China

    2

    Analysis for Design Optimization of High Thrust Liquid Engine Hot Test Facility

    10

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    8

    Development of 58N Bi-propellant thruster for Chandrayaan-2 Vikram mission

    10

    confirmed

    Mr. PRAKASH MN

    LPSC, ISRO

    India

    9

    lch4 supply scheme for engine test facilities and launch pads

    10

    confirmed

    Mr. yannick juanico

    Air Liquide

    France

    10

    Modular Engine Concept – An Economical And Versatile Solution To Future Propulsion System

    10

    confirmed

    Mr. Akira Ogawara

    Mitsubishi Heavy Industries, Ltd.

    Japan

    11

    Orion European Service Module Propulsion Subsystem after Qualification Testing prior ESM-2 Delivery and ESM-3 Integration

    10

    confirmed

    Mr. Markus Jaeger

    Airbus Defence & Space, Space Systems

    Germany

    13

    Developing a roadmap for the post-processing of additively manufactured aerospike engines

    10

    confirmed

    Mr. Maximilian Buchholz

    Technische Universität Dresden (DTU)

    Germany

    15

    hardware-in-the-loop tests of complex control software for rocket propulsion systems

    confirmed

    Dr. Günther Waxenegger-Wilfing

    DLR (German Aerospace Center)

    Germany