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  • session 1

    Title

    Propulsion System (1)

    Description

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

    Date

    2013-09-23

    Time

    15:15

    Room

    208A

    IPC members
    • Chairman: Mr. Max Calabro, The Inner Arch, France;

    • Chairman: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Rapporteur: Mr. Walter Zinner, ArianeGroup, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    The Development of LOX/LH2 Engine in China

    15'

    confirmed

    Mr. Nan Zhang

    Beijing Aerospace Propulsion Institute

    China

    2

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

    15'

    confirmed

    Mr. Weibin Wang

    China

    3

    The VINCI upper stage engine: the demonstration of maturity

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France

    4

    technology demonstration status of le-x engine

    15'

    confirmed

    Mr. Hideo Sunakawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    Cyclone-4 Launch Vehicle III stage engine. Ground testing results

    15'

    Mr. Alexandr Prokopchuk

    Yuzhnoye State Design Office

    Ukraine

    6

    Expand of Capabilities of Rocket and Space Complexes with High–Molecular Additives to Liquid Propellant Components

    15'

    confirmed

    Dr. Valeriy Gaponov

    JSC NPO Energomash

    Russian Federation

    7

    Development and Test of the LOX/Methane Regenerative Cooled Rocket Engine (2nd Report)

    15'

    confirmed

    Mr. Kohei Taya

    IHI Corporation

    Japan

    8

    Technological Demonstration Tests of main Engine for Reusable Sounding Rocket

    15'

    confirmed

    Dr. Tomoyuki Hashimoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    System analysis and applied study in the field of a choice of rocket engines for perspective reusable launchers.

    15'

    confirmed

    Mr. Yuri Gusev

    TSNIIMASH

    Russian Federation

    10

    Overview on Liquid Propulsion System Modeling Tools for Quick-Loop, Engineering and Design Studies

    15'

    confirmed

    Mr. Markus Jäger

    Astrium Space Transportation

    Germany

    11

    Propulsion Control System Model for Liquid Rocket Engines Using Intelligent Techniques

    15'

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    12

    Performance Analyses for Propulsion System of CE-2 Satellite with the Extra Missions

    15'

    confirmed

    Mr. Liang Junqiang

    Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

    China