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  • session 1

    Title

    Propulsion System (1)

    type

    oral

    Description

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

    Date

    2017-09-25

    Time

    15:15

    Room

    Hall E3

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

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

    • Rapporteur: Dr. Vanniyaperumal Narayanan, Indian Space Research Organization (ISRO), India;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Development Status of the Cryogenic Oxygen/Hydrogen YF -77 Engine for Long-March 5

    30'

    confirmed

    Mr. Dayong Zheng

    Beijing Aerospace Propulsion Institute

    China

    2

    Prometheus : European Next Generation Liquid Rocket Engine

    15'

    confirmed

    Mr. Christophe Bonhomme

    Centre National d'Etudes Spatiales (CNES)

    France

    3

    progress summary of engineering model firing tests in le-9 engine development

    15'

    confirmed

    Mr. Masaki Adachi

    Mitsubishi Heavy Industries, Ltd.

    Japan

    4

    Design and Development Status of LE-9 Engine for H3 Launch Vehicle

    15

    confirmed

    Mr. Akihide Kurosu

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    An Overview on the Turbopump Roadmap for the Lumen Demonstrator Engine and on the new Turbine Test Facility

    15'

    confirmed

    Mr. Tobias Traudt

    DLR (German Aerospace Center)

    Germany

    6

    Development Status of the 7tonf LOx/Kerosene Gas Generator Cycle Engine for KSLV-II

    15'

    confirmed

    Dr. CHANG HO NAM

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    7

    vinci engine thermo-structural composite nozzle extension for ariane 6

    15'

    confirmed

    Mr. Herve COPERET

    Airbus Safran Launchers

    France

    8

    Ignition of ADN-based monopropellants – Results of the european project RHEFORM

    15'

    confirmed

    Mr. Christian Hendrich

    DLR (German Aerospace Center)

    Germany

    9

    Prospects for use of powerful LOX-kerosene RD175 and RD176 LPRE for first stage of "Phoenix" LV of middle class and advanced LV of superheavy class.

    15'

    confirmed

    Mr. Oleg Safin

    JSC NPO Energomash

    Russian Federation

    10

    BOREAS DEMONSTRATION FOR FUTURE LIQUID PROPULSION ENGINES

    15'

    withdrawn

    Mr. Patrick Danous

    Airbus Safran Launchers

    France

    10

    Continued Development of the Aerojet Rocketdyne AR1 Staged Combustion Booster Rocket Engine

    15

    confirmed

    Mr. Tom Martin

    Aerojet Rocketdyne

    United States

    11

    Orion European Service Module Propulsion Subsystem on Fire during Qualification Testing

    15'

    confirmed

    Mr. Markus Jäger

    Airbus Defence & Space, Space Systems

    Germany

    12

    failure detection of liquid propellant rocket engine using system invariant analysis technology

    15'

    confirmed

    Dr. Masaki Sato

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    13

    AN ADDITIVELY-MANUFACTURED CNG/GOX AEROSPIKE ROCKET ENGINE: DESIGN PROCESS

    15'

    confirmed

    Mr. Graham Bell

    Monash University

    Australia