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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

    3

    Technology Demonstration Results of LE-X Engine

    15'

    withdrawn

    Mr. Shusuke Hori

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    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

    9

    modeling study on natural circulation precooling for cryogenic liquid rocket propulsion system

    15'

    withdrawn

    Mr. Shiqiang Chen

    China Academy of Launch Vehicle Technology, China

    China

    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