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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

    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

    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    withdrawn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

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

    15'

    confirmed

    Mr. Petr Levochkin

    JSC NPO Energomash

    Russian Federation

    2

    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

    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

    The Future of Liquid Propulsion: the French view

    15'

    confirmed

    Mr. Christophe Bonhomme

    Centre National d'Etudes Spatiales (CNES)

    France

    5

    Results of LE-X engine technology demonstration

    15'

    withdrawn

    Mr. Hideto Kawashima

    JAXA

    Japan

    6

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

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France

    7

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

    15'

    confirmed

    Mr. Daniele Liuzzi

    Avio Spa

    Italy

    8

    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

    Applying a Mature Green Propulsion Solution to Enhance Future Mission Capabilities

    15'

    confirmed

    Ms. Elizabeth Driscoll

    Aerojet Rocketdyne

    United States

    10

    A Novel Green Gel Propellant Based Propulsion System

    15'

    withdrawn

    Prof. Benveniste Natan

    Technion – Israel Institute of Technology

    Israel

    11

    Research on thermal decomposition of hydrogen peroxide.

    15'

    confirmed

    Dr. Lukasz Mezyk

    Warsaw University of Technology (WUT)

    Poland

    12

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

    15'

    confirmed

    Mr. Yunjae Chung

    Seoul National University

    Korea, Republic of

    13

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

    15'

    confirmed

    Prof. Chen Jianhua

    Xi'an Aerospace Propulsion Institute

    China

    14

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

    15'

    confirmed

    Mr. Vadym Khomyak

    Yuzhnoye State Design Office

    Ukraine