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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

    2012-10-01

    Time

    15:15

    Room

    TS14 (Sala Capri, Palacongressi)

    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

    SYMPOSIUM KEYNOTE: The HYPROB Program: Mastering Key Technologies, Design and Testing Capabilities for Space Transportation Rocket Propulsion Evolution

    20'

    confirmed

    2

    DEVELOPMENT OF NEW TECHNOLOGIES APPLIED TO LOX-CH4 PROPULSION

    15'

    confirmed

    Mr. Arione Luigi

    AVIO S.p.A.

    Italy

    3

    Demonstration of a 600kN class LOX/Methane Rocket Engine

    15'

    confirmed

    Prof. Nan Zhang

    Beijing Aerospace Propulsion Institute

    China

    4

    Injector Conceptions for Usage of LOX/methane Propellant Composition in Liquid-Liquid, Expander and Staged Combustion Cycles of a Liquid Rocket Engine

    15'

    no-show

    Prof. Vladimir Bazarov

    Moscow Aviation Institute (State Technical University)

    Russian Federation

    5

    OVERVIEW of LNG PROPULSION SYSTEM DEVELOPMENT

    15'

    confirmed

    Mr. Yasuhito Kano

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    Main Directions of the Pneudraulic Systems Progress of Contemporary Launch Vehicles

    15'

    confirmed

    Mr. Anatolii Lohvynenko

    Yuzhnoye State Design Office

    Ukraine

    7

    THE DEVELOPMENT AND QUALIFICATION TESTING OF THE SECOND GENERATION HIGH PERFORMANCE 490N LIQUID APOGEE ENGINE

    15'

    confirmed

    Mr. Chnagguo Liu

    China

    8

    Reusable Sounding Rocket Engine Design and Manufacturing Status of Development Engine and Components

    15'

    confirmed

    Mr. Hiromichi Hiraki

    Mitsubishi Heavy Industries, Ltd.

    Japan

    9

    Progress of the development of an all-electric control system of a rocket engine

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France

    10

    JSC "NPO Energomash named after academician V.Glushko" - Leading Russian enterprise on the development and production of liquid propellant rocket engines. Experience and prospect.

    15'

    confirmed

    Dr. Petr Levochkin

    NPO Energomash

    Russian Federation

    11

    Preliminary Design Study of Staged Combustion Cycle Rocket Engine for SpaceLiner High-Speed Passenger Transportation Concept

    Poster

    confirmed

    Mr. Ryoma Yamashiro

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    12

    Study on combustion characteristics according to recess length for a rocket engine using gas methane/lox as propellants

    Poster

    confirmed

    Mr. junsu Jeon

    Chungnam National University

    Korea, Republic of

    13

    Design Optimization of Liquid Rocket Engine using a Genetic Algorithm

    Poster

    confirmed

    Mr. Sangbok Lee

    Inha Univ.

    Korea, Republic of

    14

    Research on the cooling method for an oxygen rich preburner

    Poster

    withdrawn

    Dr. Insang Moon

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    15

    Development and test of the lox/lng regenerative cooled rocket engine

    Poster

    confirmed

    Mr. Kenichi Kimoto

    IHI Corporation

    Japan

    Technology Demonstration of Main Propulsion System for Reusable Sounding Rocket

    with 13569

    Dr. Masaki Sato

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    UPPER STAGE AND LANDING MODULE LIQUID ROCKET ENGINES WITH COMBINED STORABLE PROPELLANT SUPPLY SYSTEMS

    with 12990

    confirmed

    Dr. Vladimir Shnyakin

    Yuzhnoye State Design Office

    Ukraine