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  • session 1

    Title

    Propulsion System (1)

    Description

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

    Date

    2015-10-12

    Time

    15:15

    Room

    Ballroom B (Crowne Plaza Hotel, -1 floor)

    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;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

    The Development Plan of the First and the Second Stage Engines for the Japanese Next Flagship Launch System

    15'

    withdrawn

    Mr. Shusuke Hori

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    2

    15:30

    Creation of family of LPRE for advanced Russian and foreign launch-vehicles on the basis of RD191 engine

    15'

    confirmed

    Mr. Vladimir Sudakov

    JSC NPO Energomash

    Russian Federation

    3

    15:45

    Advancement and Future Application of Space Propulsion Technology Using Hydrocarbon Propellants in China

    15'

    confirmed

    Mr. LI Wenlong

    Xi'an Aerospace Propulsion Institute

    China

    4

    16:00

    The Future of Liquid Propulsion: the French view

    15'

    confirmed

    Mr. Christophe Bonhomme

    Centre National d'Etudes Spatiales (CNES)

    France

    5

    16:15

    Results of LE-X engine technology demonstration

    15'

    withdrawn

    Mr. Hideto Kawashima

    JAXA

    Japan

    6

    16:30

    VINCI®, the European reference for Ariane 6 upper stage cryogenic engine

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France

    7

    16:45

    Development of a LM10-MIRA LOX – LNG expander cycle Demonstrator engine

    15'

    confirmed

    Mr. Daniele Liuzzi

    Avio Spa

    Italy

    8

    17:00

    firing tests for advanced features and long-life durability of the main engine of the reusable sounding rocket

    15'

    confirmed

    Dr. Toshiya Kimura

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    17:15

    Applying a Mature Green Propulsion Solution to Enhance Future Mission Capabilities

    15'

    confirmed

    Ms. Elizabeth Driscoll

    Aerojet Rocketdyne

    United States

    10

    17:30

    A Novel Green Gel Propellant Based Propulsion System

    15'

    withdrawn

    Prof. Benveniste Natan

    Technion – Israel Institute of Technology

    Israel

    11

    17:45

    Research on thermal decomposition of hydrogen peroxide.

    15'

    confirmed

    Dr. Lukasz Mezyk

    Warsaw University of Technology (WUT)

    Poland

    12

    18:00

    Dynamic characteristics of open-type swirl injector with pulsating manifold pressure

    15'

    confirmed

    Mr. Yunjae Chung

    Seoul National University

    Korea, Republic of

    13

    18:15

    a review of china's lox/kerosene stage combustion cycle rocket engine

    15'

    confirmed

    Prof. Chen Jianhua

    Xi'an Aerospace Propulsion Institute

    China

    14

    18:30

    Features of the propellant tanks pressurization systems development of the LV upper stages

    15'

    confirmed

    Mr. Vadym Khomyak

    Yuzhnoye State Design Office

    Ukraine