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  • session 1

    Title

    Propulsion Systems I

    Description

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

    Date

    2010-09-27

    Time

    15:15

    Room

    Club A

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

    • Chairman: Prof. Vladimir Prisniakov, Russian Academy of Sciences, Ukraine;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Overview of current state of activities related to rocket propulsion R&D in Russia

    20

    Mr. Dmitry Babkin

    ROSCOSMOS

    Russian Federation

    2

    Research Progress of Reusable Liquid Rocket Engine in JAXA

    15

    confirmed

    Dr. Makoto Yoshida

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    Regenerative Cooling Cycle LOX/Methane Engine and Some Other Hydrocarbon Fueled Rocket Engine Studies

    15

    confirmed

    Mr. Kimihito Obase

    Mitsubishi Heavy Industries, Ltd.

    Japan

    4

    Development of a 35kN-Thrust-Class Closed-Cycle Hydrogen Peroxide / Kerosene Engine

    15

    Dr. Mengwei Zheng

    Beijing Aerospace Propulsion Institute

    China

    5

    progress of the vinci engine development

    15

    confirmed

    Mr. Philippe Caisso

    Safran Aircraft Engines

    France

    6

    Aerojet High-Performance Bipropellant Apogee Engines

    15

    confirmed

    Mr. Alfred Wilson

    Aerojet Rocketdyne

    United States

    7

    History and Status of Aerojet Mars Lander Propulsion Activities

    10

    confirmed

    Mr. Alfred Wilson

    Aerojet Rocketdyne

    United States

    8

    REGULATION SYSTEMS OF THE CYCLONE-4 LV UPPER STAGE MAIN LIQUID ROCKET ENGINE

    15

    confirmed

    Dr. Vladimir Shnyakin

    Yuzhnoye State Design Office

    Ukraine

    9

    Rocket propulsion using unitary paste-like propellant. Experimental investigations of paste-like propellant and results of PRM fire tests

    10

    Mr. Yulian Protsan

    The Laboratory of Advanced Jet Propulsion

    Ukraine

    10

    Hot-Fire Test of a Turbopump for a 30 Ton Class Engine

    10

    confirmed

    Dr. Soon-Sam Hong

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    11

    First Results from TP-X Turbine Tests and Verification Results from Vinci Turbines in Engine Testing

    10

    withdrawn

    Mr. Tomas Damgaard

    Volvo Aero Corporation

    Sweden