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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

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    The Development of LOX/LH2 Engine in China

    Mr. Nan Zhang

    Beijing Aerospace Propulsion Institute

    China

    2

    confirmed

    15'

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

    Mr. Weibin Wang

    China

    3

    confirmed

    15'

    The VINCI upper stage engine: the demonstration of maturity

    Mr. Patrick Danous

    Snecma

    France

    4

    confirmed

    15'

    technology demonstration status of le-x engine

    Mr. Hideo Sunakawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    15'

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

    Mr. Alexandr Prokopchuk

    Yuzhnoye State Design Office

    Ukraine

    6

    confirmed

    15'

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

    Dr. Valeriy Gaponov

    JSC NPO Energomash

    Russian Federation

    7

    confirmed

    15'

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

    Mr. Kohei Taya

    IHI Corporation

    Japan

    8

    confirmed

    15'

    Technological Demonstration Tests of main Engine for Reusable Sounding Rocket

    Dr. Tomoyuki Hashimoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    confirmed

    15'

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

    Mr. Yuri Gusev

    TSNIIMASH

    Russian Federation

    10

    confirmed

    15'

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

    Mr. Markus Jäger

    Astrium Space Transportation

    Germany

    11

    15'

    Propulsion Control System Model for Liquid Rocket Engines Using Intelligent Techniques

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    12

    confirmed

    15'

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

    Mr. Liang Junqiang

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

    China