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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

    2014-09-29

    Time

    15:15

    Room

    714B

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

    • Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    LOx/Methane Re-usable Propulsion System Development with implementation of Concurrent Engineering

    15'

    confirmed

    Mr. Paul Valton

    Airbus Defence and Space - Space Systems

    France

    2

    NASA Space Launch System Advanced Booster Risk Reduction Status Report

    15'

    confirmed

    Mr. Steve Cook

    Dynetics

    United States

    4

    numerical simulation of a lo2-ch4 rocket engine demonstrator

    15'

    confirmed

    Mr. Daniele Cardillo

    CIRA Italian Aerospace Research Center, Capua

    Italy

    5

    Development status of a 200 kN thrust Cryogenic upper stage engine for ISRO’s next generation launch vehicle

    15'

    confirmed

    Dr. Vanniyaperumal Narayanan

    Indian Space Research Organization (ISRO)

    India

    6

    Flight testing of Indian Cryogenic Upper Stage

    15'

    confirmed

    Dr. Vanniyaperumal Narayanan

    Indian Space Research Organization (ISRO)

    India

    7

    The Future of Cryogenic Propulsion

    15'

    confirmed

    Mr. Christophe Bonhomme

    Centre National d'Etudes Spatiales (CNES)

    France

    8

    Modernization of powerful LOX-kerosene LPRE of NPO Energomash by change of fuel «kerosene» on «methane»

    15'

    confirmed

    Mr. Vladimir Sudakov

    JSC NPO Energomash

    Russian Federation

    10

    Design and Demonstration Tests of LOX/LH2 Engine for Reusable Sounding Rocket

    15'

    confirmed

    Mr. Yuya FUKUDA

    Mitsubishi Heavy Industries Ltd. Japan

    Japan

    11

    student design/build/test of a throttleable lox-lch4 thrust chamber

    15'

    confirmed

    Mr. Michael Bedard

    Purdue University

    United States

    12

    The VINCI propulsion system : new steps toward qualification

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France