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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

    2016-09-26

    Time

    15:15

    Room

    Zapopan

    IPC members
    • Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Mr. Patrick Danous, ArianeGroup, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Additive Layer Manufacturing will change rocket liquid propulsion

    30'

    confirmed

    Mr. Marc Vales

    Airbus Safran Launchers

    France

    2

    overview of le-9 engine development for h3 launch vehicle

    15'

    confirmed

    Mr. Nobuki Negoro

    Mitsubishi Heavy Industries, Ltd.

    Japan

    3

    VULCAIN 2.1®, the European reference for Ariane 6 Lower stage cryogenic engine

    15'

    confirmed

    Mr. Sabin Patrick

    France

    4

    LOX/METHANE reusable rocket propulsion at reach with large scale demonstrators tested

    15'

    confirmed

    Mr. Yoan Boué

    Airbus Safran Launchers

    France

    5

    Effect of bearing supporting stiffness on critical speed and dynamic stability of turbo-pump rotor system in LOX/Kerosene rocket engine

    15'

    confirmed

    Dr. Feiping Du

    Xi'an Aerospace Propulsion Institute

    China

    6

    Challenges in restart of pressure fed liquid upper stage

    15'

    confirmed

    Dr. Deepak Kumar Agarwal

    LPSC, ISRO

    India

    7

    Leveraging Additive Manufacturing for Affordable Commercial Launch Applications Enabled by the Aerojet Rocketdyne Ultra-Low-Cost Bantam Engine Family

    15'

    confirmed

    Dr. Jerrol Littles

    Aerojet Rocketdyne

    United States

    8

    Vinci® Propulsion System: Transition from Ariane 5 ME to Ariane 6

    15'

    confirmed

    Mr. Patrick Danous

    Snecma

    France

    9

    Development of an up-rated version of earth storable pump fed liquid engine for ISRO launch vehicles.

    15'

    withdrawn

    Mr. Aneesh Rajan

    LPSC, ISRO

    India

    10

    static characteristic analysis of 180kn lox/kerosene upper stage engine

    '15

    confirmed

    Dr. Yuanqi Li

    Xian Aerospace Propulsion Institute

    China

    11

    Development status of CE20 cryogenic engine for GSLV LVM3 vehicle

    '15

    no-show

    Dr. Vanniyaperumal Narayanan

    Indian Space Research Organization (ISRO)

    India

    12

    Multidiscipline approach to the design and modernization of high power Liquid Propellant Engines for their reuse

    15'

    withdrawn

    Mr. Vladimir Tkach

    JSC NPO Energomash

    Russian Federation

    13

    effect of fuel injection schemes in a vortex combustion chamber

    '15

    no-show

    Mr. Vikash Kumar

    Liquid Propulsion System centre

    India

    14

    The design and test of 250N thruster with HAN-based propellant

    '15

    confirmed

    Mr. xin Qiu

    Shanghai Institute of Space Propulsion

    China

    15

    Multidisciplinary design optimization of a spacecraft bi-propellant propulsion system using a computationally improved framework

    15'

    withdrawn

    Mr. H.R. Fazeley

    K. N. Toosi University of Technology

    Iran