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  • session 1

    Title

    Liquid Propulsion (1)

    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: 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

    2

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

    14

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    3

    Prospects for use of upgraded RD-180 engine in Russian programs for creation of launch-vehicles of new generation

    14

    Mr. Petr Levochkin

    NPO Energomash

    Russian Federation

    4

    Low-Cost Manufacturing Technologies of Commercial Liquid Rocket Engine (LRE) and Rapid Implementation of Hot-Fire Test System for the Chinese First Metha-LOX LRE Development

    14

    Mr. Ruikang Yang

    LandSpace Technology

    China

    5

    Research Activities in the Development of DemoP1: a LOX/LNG Aerospike Engine Demonstrator

    14

    withdrawn

    Mr. adria argemi

    Spain

    6

    Qualification test results of LE-9 engine for H3 launch vehicle

    14

    Mr. Hideto Kawashima

    JAXA

    Japan

    7

    Comparison of Rocket Engine Cooling Channel Geometries Enabled by Additive Manufacturing

    14

    Mr. Nick Salamon

    The Ohio State University College of Engineering

    United States

    8

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

    14

    confirmed

    Mr. PRAKASH MN

    LPSC, ISRO

    India

    9

    lch4 supply scheme for engine test facilities and launch pads

    14

    confirmed

    Mr. yannick juanico

    Air Liquide

    France

    10

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

    14

    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

    14

    confirmed

    Mr. Markus Jaeger

    Airbus Defence & Space, Space Systems

    Germany

    12

    test results from the all additively manufactured prometheus turbine

    14

    Mr. Staffan Brodin

    GKN Aerospace Engine Systems

    Sweden

    13

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

    confirmed

    Mr. Maximilian Buchholz

    Dresden University of Technology (DUT) / Technische Universität Dresden

    Germany

    14

    Cyclic stress analysis of Semicryo engine thrust chamber using Chaboche unified viscoplastic model

    Dr. Ahmedul Asraff

    Liquid Propulsion Systems Centre(LPSC), Indian Space Research Organization (ISRO)

    India

    15

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

    Dr. Günther Waxenegger-Wilfing

    DLR (German Aerospace Center)

    Germany